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• NASA-96-cr201633
  • EXPERIMENTAL AND COMPUTATIONAL AEROTHERMODYNAMICS OF A MARS ENTRY VEHICLE
  • ABSTRACT
  • BIOGRAPHY
  • ACKNOWLEDGMENTS
  • ACKNOWLEDGMENTS-continue
  • TABLE OF CONTENTS
  • TABLE OF CONTENTS-continue
  • TABLE OF CONTENTS-continue
  • LIST OF TABLES
  • LIST OF TABLES-continue
  • LIST OF TABLES-continue
  • LIST OF TABLES-continue
  • LIST OF TABLES-continue
  • LIST OF FIGURES
  • LIST OF FIGURES-continue
  • LIST OF FIGURES-continue
  • LIST OF FIGURES-continue
  • LIST OF FIGURES-continue
  • LIST OF FIGURES-continue
  • LIST OF FIGURES-continue
  • LIST OF FIGURES-continue
  • LIST OF FIGURES-continue
  • LIST OF FIGURES-continue
  • LIST OF FIGURES-continue
  • LIST OF FIGURES-continue
  • LIST OF FIGURES-continue
  • LIST OF FIGURES-continue
  • LIST OF FIGURES-continue
  • LIST OF FIGURES-continue
  • LIST OF FIGURES-continue
  • LIST OF FIGURES-continue
  • LIST OF SYMBOLS
  • LIST OF SYMBOLS-continue
  • LIST OF SYMBOLS-continue
  • LIST OF SYMBOLS-continue
  • CHAPTER 1 INTRODUCTION
  • AEROBRAKING AND AEROASSISTED ORBIT TRANSFER
  • AEROBRAKING AND MARS EXPLORATION MISSIONS
  • BLUNT-BODY AEROBRAKE WAKE FLOW
  • BLUNT-BODY AEROBRAKE WAKE FLOW-continue
  • DESCRIPTION OF RESEARCH
  • DESCRIPTION OF RESEARCH-continue
  • DESCRIPTION OF RESEARCH-continue
  • Figure 1.3.1 Mars Viking Geometry
  • Figure1.3.2 Mars Pathfinder Geometry
  • Figure 1.4.1 Blunt-Body Wake Flow Structure
  • Figure 1.4.2 Aeroassist Flight Experiment (AFE) Vehicle
  • CHAPTER 2 LITERATURE REVIEW
  • Experimental studies
  • Experimental studies-continue
  • Experimental studies-continue
  • Experimental studies-continue
  • Experimental studies-continue
  • Computational studies
  • Computational studies-continue
  • Computational studies-continue
  • CHAPTER 3 MODEL DESIGN AND INSTRUMENTATION
  • Model Configurations
  • Model Construction
  • Model Construction-continue
  • Model Construction-continue
  • Model Instrumentation
  • Model Instrumentation-continue
  • Model Instrumentation-continue
  • Gage Calibration
  • Gage Calibration-continue
  • Gage Calibration-continue
  • Figure 3.1.1 MP-1 Geometry
  • Figure 3.1.2 MP-1 Model and Sting
  • Figure 3.1.3 Parametric Entry Vehicle configurations
  • Figure 3.1.4 MP-1 and MP-2 Configurations
  • Figure 3.1.5 Scaled Stainless-Steel MP-1 Models
  • Figure 3.2.1 Semi-Infinite Test Time vs. Substrate Thickness
  • Figure 3.3.1 Thin-film Gage Details
  • Figure 3.3.2 Thin-Film Gage Layout on MP-1 Model
  • Figure 3.3.3 Thin Film Gage Layout on 1-in. Radius Hemispheres
  • Figure 3.3.4 Thin Film Gage Layout on 1/4-in., 3/8-in. and 1/2-in. Rad. Hemispheres
  • Figure 3.4.1 Typical Thin-Film Gage Voltage-Temperature Calibration
  • CHAPTER 4 EXPERIMENTAL FACILITIES
  • NASA Langley 31-Inch Mach 10 Air Tunnel
  • Flow Conditions
  • NASA HYPULSE Expansion Tube
  • Facility Description
  • Facility Description-continue
  • Flow Conditions and Test Times
  • Flow Conditions and Test Times-continue
  • Flow Conditions and Test Times-continue
  • Flow Conditions and Test Times-continue
  • Table 4.2.1 Flow Conditions for the NASA Langley 31-Inch Mach 10 Air Tunnel
  • Table 4.3.1 Flow Conditions for the NASA HYPULSE Expansion Tube
  • Figure 4.1.1 NASA Langley 31-Inch Mach 10 Air Tunnel
  • Figure 4.1.2 NASA HYPULSE Expansion Tube
  • Figure 4.2.1 Schematic of NASA Langley 31-Inch Mach 10 Air Tunnel
  • Figure 4.2.2 NASA Langley 31-Inch Mach 10 Air Tunnel Pitot Calibration
  • Figure 4.3.1 Schematic of NASA HYPULSE Expansion Tube
  • Figure 4.3.2 X-T Diagram for NASA HYPULSE Expansion Tube
  • Figure 4.3.3 Typical HYPULSE Wall Pressure Time History
  • Figure 4.3.4 Typical CO2 Test Window
  • Figure 4.3.5 Typical Air Test Window
  • CHAPTER 5 DATA ACQUISITION AND REDUCTION
  • Analytical Techniques
  • Analytical Techniques-continue
  • Analytical Techniques-continue
  • Numerical Techniques
  • Numerical Techniques-continue
  • Numerical Techniques-continue
  • Numerical Techniques-continue
  • Figure 5.2.1 Sensor and One-Dimensional Semi-Infinite Substrate
  • Figure 5.2.2 Sample 31-Inch Mach 10 Heating Data
  • Figure 5.2.3 Finite-Volume Energy Balance and Nomenclature
  • Figure 5.2.4 Comparison of Heat Transfer Data Reduction Techniques
  • CHAPTER 6 EXPERIMENTAL RESULTS
  • CHAPTER 6 EXPERIMENTAL RESULTS-continue
  • 31-Inch Mach 10 Air Tunnel Data
  • Reynolds Number Effects
  • Reynolds Number Effects-continue
  • Angle-of-Attack Effects
  • Configuration Effects
  • Configuration Effects-continue
  • Transition Grit Effects
  • Repeatability
  • HYPULSE Expansion Tube Data
  • Wake Flow Establishment
  • Wake Flow Establishment-continue
  • Wake Flow Establishment-continue
  • Wake Flow Establishment-continue
  • Repeatability and Averaged Heating Distributions
  • Angle-of-Attack Effects
  • Configuration Effects
  • Configuration Effects-continue
  • Test Gas Effects and Comparison with Perfect Gas Data
  • Uncertainty Analysis
  • Uncertainty Analysis
  • Uncertainty Analysis-continue
  • Uncertainty Analysis-continue
  • Uncertainty Analysis-continue
  • Table 6.2.1 MP-1 Configuration, CO2 Test Gas, α= 0 deg
  • Table 6.2.2 MP-1 Configuration, CO2 Test Gas, α= -4 deg
  • Table 6.2.3 MP-1 Configuration, Air Test Gas, α= 0 deg
  • Table 6.2.4 MP-1 Configuration, Air Test Gas, α= -4 deg
  • Table 6.2.5 MP-2 Configuration, CO2 Test Gas, α= 0 deg
  • Table 6.2.6 MP-2 Configuration, CO2 Test Gas, α= -4 deg
  • Table 6.2.7 MP-2 Configuration, Air Test Gas, α= 0 deg
  • Table 6.2.8 MP-3 Configuration, CO2 Test Gas, α= 0 deg
  • Table 6.2.9 MP-4 Configuration, CO2 Test Gas, α= 0 deg
  • Figure 6.0.1 Surface Control Points on Entry Vehicle Models
  • Figure 6.0.2 Typical Entry Vehicle CH Data
  • Figure 6.1.1b Reynolds Number Effects on MP-1 Configuration
  • Figure 6.1.2a Reynolds Number Effects on MP-2 Configuration
  • Figure 6.1.3b Reynolds Number Effects on MP-3 Configuration
  • Figure 6.1.4a Reynolds Number Effects on MP-4 Configuration
  • Figure 6.1.5 Oil Flow Patterns on MP-1 Configuration
  • Figure 6.1.6 Oil Flow Patterns on MP-1 Configuration
  • Figure 6.1.7 Oil Flow Patterns on MP-1 Configuration
  • Figure 6.1.8 Reynolds Number Effects on Sting Peak CH Location
  • Figure 6.1.9a α Effects on MP-1 Configuration
  • Figure 6.1.10a MP-1 CH Distributions, α= -4 deg.
  • Figure 6.1.11a MP-1 CH Distributions, α= -12 deg
  • Figure 6.1.12b MP-1 CH Distributions, α= -20 deg
  • Figure 6.1.13a α Effects on MP-2 Configuration
  • Figure 6.1.14b α Effects on MP-3 Configuration
  • Figure 6.1.15a α Effects on MP-4 Configuration
  • Figure 6.1.16 α Effects on Sting Peak CH Location
  • Figure 6.1.17b Configuration Effects on Wake, α = 0 deg
  • Figure 6.1.18a Configuration Effects on Forebody, α = 0 deg
  • Figure 6.1.19b Configuration Effects on Wake, α = 0 deg
  • Figure 6.1.20a Configuration Effects on Forebody, α = -4 deg
  • Figure 6.1.21b Configuration Effects on Wake, α = -20 deg
  • Figure 6.1.22a Transition Grit Effects, MP-1 Configuration
  • Figure 6.1.22c Transition Grit Effects, MP-1 Configuration
  • Figure 6.1.23a Repeatability, MP-1 Configuration
  • Figure 6.1.24a Repeatability, MP-2 Configuration
  • Figure 6.1.25a Repeatability, MP-3 Configuration
  • Figure 6.1.26a Repeatability, MP-4 Configuration
  • Figure 6.2.1a Wake Flow Establishment Movie, Run 749: 0 to 60 µsec
  • Figure 6.2.1d Wake Flow Establishment Movie, Run 749: 180 to 240 µsec
  • Figure 6.2.1e Wake Flow Establishment Movie, Run 749: 240 to 300 µsec
  • Figure 6.2.2 Wall Pressure Time History, Run 749
  • Figure 6.2.4a MP-1 Configuration, α = 0 deg, CO2 in HYPULSE
  • Figure 6.2.5a MP-1 Configuration, α = -4 deg, CO2 in HYPULSE
  • Figure 6.2.6a MP-1 Configuration, α = 0 deg, Air in HYPULSE
  • Figure 6.2.7a MP-1 Configuration, α = -4 deg, Air in HYPULSE
  • Figure 6.2.8a MP-2 Configuration, α = 0 deg, CO2 in HYPULSE
  • Figure 6.2.9a MP-2 Configuration, α = -4 deg, CO2 in HYPULSE
  • Figure 6.2.10a MP-2 Configuration, α = 0 deg, Air in HYPULSE
  • Figure 6.2.11b MP-3 Configuration, α = 0 deg, CO2 in HYPULSE
  • Figure 6.2.12a MP-4 Configuration, α = 0 deg, CO2 in HYPULSE
  • Figure 6.2.13a α Effects on MP-1 Configuration, CO2 in HYPULSE
  • Figure 6.2.14b α Effects on MP-1 Configuration, Air in HYPULSE
  • Figure 6.2.15a α Effects on MP-2 Configuration, CO2 in HYPULSE
  • Figure 6.2.16a Configuration Effects on Forebody, α = 0 deg, CO2 in HYPULSE
  • Figure 6.2.17a Configuration Effects on Forebody, α = 0 deg, Air in HYPULSE
  • Figure 6.2.18a Configuration Effects on Forebody, α = -4 deg, CO2 in HYPULSE
  • Figure 6.2.19b Comparison of Mach 10 and HYPULSE Data, MP-1 Wake
  • Figure 6.2.20a Comparison of Mach 10 and HYPULSE Data, MP-2 Forebody
  • Figure 6.2.21a Comparison of Mach 10 and HYPULSE Data, MP-3 Forebody
  • Figure 6.2.22a Comparison of Mach 10 and HYPULSE Data, MP-4 Forebody
  • Figure 6.3.1a MP-1 Forebody Uncertainty Estimates, Re=1.0x106 ft-1 in Mach 10
  • Figure 6.3.2b MP-1 Wake Uncertainty Estimates, CO2 in HYPULSE
  • Figure 6.3.3b MP-1 Wake Uncertainty Estimates, Air in HYPULSE
  • CHAPTER 7 COMPUTATIONAL TECHNIQUES
  • Formulation of Governing Equations
  • Formulation of Governing Equations-continue
  • Formulation of Governing Equations-continue
  • Transformation of Governing Equations
  • Transformation of Governing Equations-continue
  • Transformation of Governing Equations-continue
  • NEQ2D Navier-Stokes Solver
  • NEQ2D Navier-Stokes Solver-continue
  • NEQ2D Navier-Stokes Solver-continue
  • NEQ2D Navier-Stokes Solver-continue
  • NEQ2D Navier-Stokes Solver-continue
  • Grid Generation and Adaptation
  • Grid Generation and Adaptation-continue
  • Grid Generation and Adaptation-continue
  • Grid Generation and Adaptation-continue
  • Grid Generation and Adaptation-continue
  • Grid Generation and Adaptation-continue
  • Grid Generation and Adaptation-continue
  • Grid Generation and Adaptation-continue
  • Grid Generation and Adaptation-continue
  • Grid Generation and Adaptation-continue
  • Figure 7.3.1 Mach Contours Superimposed on Original and Shock-Aligned Grids
  • Figure 7.3.2 Shock Aligned Point Grids Before and After Shear Layer Adaptation
  • Figure 7.3.3 Mach Contours from Solutions on original and Shear-Layer Adapted Grids
  • Figure 7.3.4 Streamlines from Solutions and Original and Shear-Layer Adapted Grids
  • CHAPTER 8 COMPUTATIONAL RESULTS AND COMPARISONS WITH EXPERIMENTAL DATA
  • 31-Inch Mach 10 Air Tunnel Test Conditions
  • 31-Inch Mach 10 Air Tunnel Test Conditions-continue
  • Computed Flow Fields and Surface Distributions
  • Computed Flow Fields and Surface Distributions-continue
  • Computed Flow Fields and Surface Distributions-continue
  • Computed Flow Fields and Surface Distributions-continue
  • Reynolds Number Effects
  • Configuration Effects
  • Comparison with Experimental Data
  • Comparison with Experimental Data-continue
  • Comparison with Experimental Data-continue
  • Comparison with Experimental Data-continue
  • HYPULSE Expansion Tube Test Conditions
  • Computed Flow Fields and Surface Distributions
  • Computed Flow Fields and Surface Distributions-continue
  • Computed Flow Fields and Surface Distributions-continue
  • Test Gas and Configuration Effects
  • Comparison with Perfect-Gas Computations
  • Comparison with Experimental Data
  • Comparison with Experimental Data-continue
  • Figure 8.1.1 Computational Grid, MP-1 Configuration, 31-Inch Mach 10 Air Tunnel Tests
  • Figure 8.1.2 Computational Grid, MP-1 Configuration, Forebody and Near Wake Details
  • Figure 8.1.3a Grid Resolution Effects on Wake Pressure MP-1 Configuration
  • Figure 8.1.4a Grid Resolution Effects on Forebody Heating, MP-1 Configuration
  • Figure 8.1.5b Grid Resolution Effects on Wake Pressure, MP-1 Configuration
  • Figure 8.16b Grid Resolution Effects on Wake Heating, MP-1 Configuration
  • Figure 8.1.7a Grid Resolution Effects on Forebody Pressure, MP-1 Configuration
  • Figure 8.1.8b Grid Resolution Effects on Wake Heating, MP-1 Configuration
  • Figure 8.1.9 Computed Streamlines, MP-1 Configuration, 31-Inch Mach 10
  • Figure 8.1.10 Computed Streamlines Superimposed on v-Velocity Contours
  • Figure 8.1.11 Computed Mach Contours, MP-1 Configuration, 31-Inch Mach 10
  • Figure 8.1.12 Computed Pressure Ratio Contours, MP-1 Configuration
  • Figure 8.1.13 Computed Temperature Contours
  • Figure 8.1.14 Computed Density Ratio Contours
  • Figure 8.1.15 Computed Local Knudsen Number Contours
  • Figure 8.1.16 Computed Streamlines, MP-1 Configuration, 31-Inch Mach 10
  • Figure 8.1.17 Computed Streamlines Superimposed on v-Velocity Contours
  • Figure 8.1.18 Computed Mach Contours, MP-1 Configuration, 31 Inch Mach 10
  • Figure 8.1.19 Computed Pressure Ratio Contours
  • Figure 8.1.20 Computed Temperature Contours
  • Figure 8.1.21 Computed Density Ratio Contours
  • Figure 8.1.22 Computed Local Knudsen Number Contours
  • igure 8.1.23 Computed Streamlines
  • Figure 8.1.24 Computed Streamlines Superimposed on v-Velocity Contours
  • Figure 8.1.25 Computed Mach Contours, MP-1 Configuration, 31-Inch Mach 10
  • Figure 8.1.26 Computed Pressure Ratio Contours
  • Figure 8.1.27 Computed Temperature Contours
  • Figure 8.1.28 Computed Density Ratio Contours
  • Figure 8.1.29 Computed Local Knudsen Number Contours
  • Figure 8.1.30 Comparison of Computed Streamline with Surface Oil Flow Patterns
  • Figure 8.1.31 Computed Surface Pressure Distribution
  • Figure 8.1.32 Computed Surface Heating Distribution,
  • Figure 8.1.33 Computed Surface Pressure Distribution
  • Figure 8.1.34 Computed Surface Heating Distribution
  • Figure 8.1.35 Computed Surface Pressure Distribution
  • Figure 8.1.36 Computed Surface Heating Distribution
  • Figure 8.1.37 Computed Surface Pressure Distribution, MP-2 Configuration, 31-Inch Mach 10
  • Figure 8.1.38 Computed Surface Heating Distribution, MP-2 Configuration
  • Figure 8.1.39 Computed Surface Pressure Distribution MP-2 Configuration
  • Figure 8.1.40 Computed Surface Heating Distribution, MP-2 Configuration
  • Figure 8.1.41 Computed Surface Pressure Distribution, MP-2 Configuration
  • Figure 8.1.42 Computed Surface Heating Distribution, MP-2 Configuration
  • Figure 8.1.43 Computed Surface Pressure Distribution, MP-3 Configuration
  • Figure 8.1.44 Computed Surface Heating Distribution, MP-3 Configuration
  • Figure 8.1.45 Computed Surface Pressure Distribution, MP-3 Configuration
  • Figure 8.1.46 Computed Surface Heating Distribution, MP-3 Configuration
  • Figure 8.1.47 Computed Surface Pressure Distribution, MP-3 Configuration
  • igure 8.1.48 Computed Surface Heating Distribution, MP-3 Configuration
  • Figure 8.1.49 Computed Surface Pressure Distribution, MP-4 Configuration
  • Figure 8.1.50 Computed Surface Heating Distribution, MP-4 Configuration
  • Figure 8.1.51 Computed Surface Pressure Distribution, MP-4 Configuration
  • Figure 8.1.52 Computed Surface Heating Distribution, MP-4 Configuration
  • Figure 8.1.53 Computed Surface Pressure Distribution, MP-4 Configuration
  • Figure 8.1.54 Computed Surface Heating Distribution, MP-4 Configuration
  • Figure 8.1.55a Reynolds Number Effects on Forebody Heating, MP-1 Configuration
  • Figure 8.1.56a Reynolds Number Effects on Forebody Heating, MP-2 Configuration
  • Figure 8.1.57b Reynolds Number Effects on Wake Heating, MP-3 Configuration
  • Figure 8.1.58a Reynolds Number Effects on Forebody Heating, MP-4 Configuration
  • Figure 8.1.59 Reynolds Number Effects on Sting Peak Heating Location
  • Figure 8.1.60a Configuration Effects on Forebody Heating, 31-Inch Mach 10
  • Figure 8.1.61b Configuration Effects on Wake Heating, 31-Inch Mach 10
  • Figure 8.1.62b Configuration Effects on Wake Heating, 31-Inch Mach 10
  • Figure 8.1.63a Comparison with Experimental Forebody Heating Distribution, MP-1 Configuration
  • igure 8.1.64b Comparison with Experimental Wake Heating Distribution, MP-1 Configuration
  • Figure 8.1.65a Comparison with Experimental Forebody Heating Distribution, MP-1 Configuration
  • Figure 8.1.66a Comparison with Experimental Forebody Heating Distribution, MP-2 Configuration
  • Figure 8.1.67a Comparison with Experimental Forebody Heating Distribution, MP-2 Configuration
  • Figure 8.1.68a Comparison with Experimental Forebody Heating Distribution, MP-2 Configuration
  • Figure 8.1.69a Comparison with Experimental Forebody Heating Distribution, MP-3 Configuration
  • Figure 8.1.70a Comparison with Experimental Forebody Heating Distribution, MP-3 Configuration
  • Figure 8.1.71a Comparison with Experimental Forebody Heating Distribution, MP-3 Configuration
  • Figure 8.1.72a Comparison with Experimental Forebody Heating Distribution, MP-4 Configuration
  • Figure 8.1.73a Comparison with Experimental Forebody Heating Distribution, MP-4 Configuration
  • Figure 8.1.74b Comparison with Experimental Wake Heating Distribution, MP-4 Configuration
  • Figure 8.1.75 Transition to Turbulence in Wake
  • Figure 8.2.1 Computational Grid, MP-1 Configuration HYPULSE, CO2
  • Figure 8.2.2 Computational Grid, MP-1 Configuration, Forebody and Near Wake Details, HYPULSE, CO2
  • Figure 8.2.3 Computational Grid, MP-1 Configuration HYPULSE, Air
  • Figure 8.2.4 Computational Grid, MP-1 Configuration, Forebody and Near Wake Details, HYPULSE, Air
  • Figure 8.2.5a Grid Resolution Effects on Forebody Pressure, MP-1 Configuration, HYPULSE, CO2
  • Figure 8.2.6a Grid Resolution Effects on Forebody Heating, MP-1 Configuration, HYPULSE, CO2
  • Figure 8.2.7a Grid Resolution Effects on Forebody Pressure, MP-1 Configuration, HYPULSE, Air
  • Figure 8.2.8b Grid Resolution Effects on Wake Heating, MP-1 Configuration, HYPULSE, Air
  • Figure 8.2.9 Computed Streamlines, MP-1 Configuration, HYPULSE, CO2
  • Figure 8.2.10 Computed Streamlines Superimposed on v-Velocity Contours, MP-1 Configuration
  • Figure 8.2.11 Computed Mach Contours, MP-1 Configuration, HYPULSE, CO2
  • Figure 8.2.12 Computed Pressure Ratio Contours, MP-1 Configuration, HYPULSE, CO2
  • Figure 8.2.13 Computed Temperature Contours, MP-1 Configuration, HYPULSE, CO2
  • Figure 8.2.14 Computed T/Tv Contours, MP-1 Configuration, HYPULSE, CO2
  • Figure 8.2.15 Computed Density Ratio Contours, MP-1 Configuration, HYPULSE, CO2
  • Figure 8.2.16 Computed Local Knudsen Number Contours, MP-1 Configuration, HYPULSE, CO2
  • Figure 8.2.17 Computed X(CO2) Mass Fraction Contours, MP-1 Configuration, HYPULSE, CO2
  • Figure 8.2.18 Computed X(CO) Mass Fraction Contours, MP-1 Configuration, HYPULSE, CO2
  • Figure 8.2.19 Computed X(O2) Mass Fraction Contours, MP-1 Configuration, HYPULSE, CO2
  • Figure 8.2.20 Computed X(O) Mass Fraction Contours, MP-1 Configuration, HYPULSE, CO2
  • Figure 8.2.21 Computed Streamlines, MP-1 Configuration, HYPULSE, Air
  • Figure 8.2.22 Computed Streamlines Superimposed on v-Velocity Contours, MP-1 Configuration, HYPULSE, Air
  • Figure 8.2.23 Computed Mach Contours, MP-1 Configuration, HYPULSE, Air
  • Figure 8.2.24 Computed Pressure Ratio Contours, MP-1 Configuration, HYPULSE, Air
  • Figure 8.2.25 Computed Temperature Contours, MP-1 Configuration, HYPULSE, Air
  • Figure 8.2.26 Computed T/Tv Contours, MP-1 Configuration, HYPULSE, Air
  • Figure 8.2.27 Computed Density Ratio Contours, MP-1 Configuration, HYPULSE, Air
  • Figure 8.2.28 Computed Local Knudsen Number Contours, MP-1 Configuration, HYPULSE, Air
  • igure 8.2.29 Computed X(N2) Contours, MP-1 Configuration, HYPULSE, Air
  • Figure 8.2.30 Computed X(O2) Contours, MP-1 Configuration, HYPULSE, Air
  • Figure 8.2.31 Computed X(NO) Contours, MP-1 Configuration, HYPULSE, Air
  • Figure 8.2.32 Computed X(O) Contours, MP-1 Configuration, HYPULSE, Air
  • Figure 8.2.33 Computed Surface Pressure Distribution, MP-1 Configuration, HYPULSE, CO2
  • Figure 8.2.34 Computed Surface Heating Distribution, MP-1 Configuration, HYPULSE, CO2
  • Figure 8.2.35 Computed Surface Pressure Distribution, MP-1 Configuration, HYPULSE, Air
  • Figure 8.2.36 Computed Surface Heating Distribution, MP-1 Configuration, HYPULSE, Air
  • Figure 8.2.37 Computed Surface Pressure Distribution, MP-2 Configuration, HYPULSE, CO2
  • Figure 8.2.38 Computed Surface Heating Distribution, MP-2 Configuration, HYPULSE, CO2
  • igure 8.2.39 Computed Surface Pressure Distribution, MP-3 Configuration, HYPULSE, CO2
  • Figure 8.2.40 Computed Surface Heating Distribution, MP-3 Configuration, HYPULSE, CO2
  • Figure 8.2.41 Computed Surface Pressure Distribution, MP-4 Configuration, HYPULSE, O2
  • Figure 8.2.42 Computed Surface Heating Distribution, MP-4 Configuration, HYPULSE, CO2
  • Figure 8.2.43b Test Gas Effects on Wake Heating Distributions, MP-1 Configuration, HYPULSE
  • Figure 8.2.44b Configuration Effects on Wake Heating Distributions, HYPULSE, CO2
  • Figure 8.2.45a Comparison of Computed Mach 10 and HYPULSE Heating Distributions, MP-1 Forebody
  • Figure 8.2.46b Comparison of Computed Mach 10 and HYPULSE Heating Distributions, MP-2 Wake
  • Figure 8.2.47b Comparison of Computed Mach 10 and HYPULSE Heating Distributions, MP-3 Wake
  • Figure 8.2.48a Comparison of Computed Mach 10 and HYPULSE Heating Distributions, MP-4 Forebody
  • Figure 8.2.49 Comparison of Computed Mach 10 and HYPULSE Pressure Distributions, MP-1 Forebody
  • Figure 8.2.50b Comparison with Experimental Wake Heating Distribution, MP-1 Configuration, HYPULSE, CO2
  • Figure 8.2.51a Comparison with Experimental Forebody Heating Distribution, MP-1 Configuration
  • Figure 8.2.52b Comparison with Experimental Wake Heating Distribution, MP-2 Configuration
  • Figure 8.2.53b Comparison with Experimental Wake Heating Distribution, MP-3 Configuration
  • Figure 8.2.54b Comparison with Experimental Wake Heating Distribution, MP-4 Configuration
  • Figure 8.2.55b Normalized Comparison with Experimental Wake Heating Distribution, MP-1 Configuration
  • Figure 8.2.56b Normalized Comparison with Experimental Wake Heating Distribution MP-1 Configuration
  • Figure 8.2.57a Normalized Comparison with Experimental Forebody Heating Distribution, MP-2 Configuration
  • Figure 8.2.58b Normalized Comparison with Experimental Wake Heating Distribution, MP-3 Configuration
  • Figure 8.2.59a Normalized Comparison with Experimental Forebody Heating Distribution, MP-4 Configuration
  • CHAPTER 9 SUMMARY, CONCLUSIONS AND RECOMMENDATIONS
  • CHAPTER 9 SUMMARY, CONCLUSIONS AND RECOMMENDATIONS-continue
  • CHAPTER 9 SUMMARY, CONCLUSIONS AND RECOMMENDATIONS-continue
  • CHAPTER 9 SUMMARY, CONCLUSIONS AND RECOMMENDATIONS-continue
  • CHAPTER 9 SUMMARY, CONCLUSIONS AND RECOMMENDATIONS-continue
  • CHAPTER 9 SUMMARY, CONCLUSIONS AND RECOMMENDATIONS-continue
  • CHAPTER 9 SUMMARY, CONCLUSIONS AND RECOMMENDATIONS-continue
  • CHAPTER 9 SUMMARY, CONCLUSIONS AND RECOMMENDATIONS-continue
  • CHAPTER 10 REFERENCES
  • CHAPTER 10 REFERENCES-continue
  • CHAPTER 10 REFERENCES-continue
  • CHAPTER 10 REFERENCES-continue
  • CHAPTER 10 REFERENCES-continue
  • CHAPTER 10 REFERENCES-continue
  • CHAPTER 10 REFERENCES-continue
  • CHAPTER 10 REFERENCES-continue
  • CHAPTER 10 REFERENCES-continue
  • CHAPTER 10 REFERENCES-continue
  • APPENDIX A: 31 INCH MACH 10 AIR TUNNEL DATA
  • APPENDIX A: 31 INCH MACH 10 AIR TUNNEL DATA-continue
  • TABLE A.1 31-Inch Mach 10 Test 293 Run Matrix
  • TABLE A.2 31-Inch Mach 10 Test 293 Flow Conditions
  • TABLE A.3 31-Inch Mach 10 Test 307 Run Matrix
  • TABLE A.4 31-Inch Mach 10 Test 307 Flow Conditions
  • TABLE A.5 31-Inch Mach 10 Test 293, Run 005 Heating Data MP-1 Configuration
  • TABLE A.6 31-Inch Mach 10 Test 293, Run 006 Heating Data MP-1 Configuration
  • TABLE A.7 31-Inch Mach 10 Test 293, Run 007 Heating Data MP-1 Configuration
  • TABLE A.8 31-Inch Mach 10 Test 293, Run 008 Heating Data MP-1 Configuration
  • TABLE A.9 31-Inch Mach 10 Test 293, Run 009 Heating Data MP-1 Configuration
  • TABLE A.10 31-Inch Mach 10 Test 293, Run 010 Heating Data MP-1 Configuration
  • TABLE A.14 31-Inch Mach 10 Test 293, Run 014 Heating Data MP-2 Configuration
  • TABLE A.12 31-Inch Mach 10 Test 293, Run 012 Heating Data MP-2 Configuration
  • TABLE A.13 31-Inch Mach 10 Test 293, Run 013 Heating Data MP-2 Configuration
  • TABLE A.14 31-Inch Mach 10 Test 293, Run 014 Heating Data MP-2 Configuration
  • TABLE A.15 31-Inch Mach 10 Test 293, Run 015 Heating Data MP-2 Configuration
  • TABLE A.16 31-Inch Mach 10 Test 293, Run 016 Heating Data MP-2 Configuration
  • TABLE A.17 31-Inch Mach 10 Test 293, Run 017 Heating Data MP-3 Configuration
  • TABLE A.18 31-Inch Mach 10 Test 293, Run 018 Heating Data Mp-3 Configuration
  • TABLE A.19 31-Inch Mach 10 Test 293, Run 019 Heating Data MP-3 Configuration
  • TABLE A.20 31-Inch Mach 10 Test 293, Run 020 Heating Data MP-3 Configuration
  • TABLE A.21 31-Inch Mach 10 Test 293, Run 021 Heating Data MP-3 Configuration
  • TABLE A.22 31-Inch Mach 10 Test 293, Run 022 Heating Data MP-3 Configuration
  • TABLE A.23 31-Inch Mach 10 Test 293, Run 023 Heating Data MP-4 Configuration
  • TABLE A.24 31-Inch Mach 10 Test 293, Run 024 Heating Data MP-4 Configuration
  • TABLE A.25 31-Inch Mach 10 Test 293, Run 025 Heating Data MP-4 Configuration
  • TABLE A.26 31-Inch Mach 10 Test 293, Run 026 Heating Data MP-4 Configuration
  • TABLE A.27 31-Inch Mach 10 Test 293, Run 027 Heating Data MP-4 Configuration
  • TABLE A.28 31-Inch Mach 10 Test 293, Run 028 Heating Data MP-4 Configuration
  • TABLE A.29 31-Inch Mach 10 Test 293, Run 029 Heating Data MP-1 Configuration
  • TABLE A.30 31-Inch Mach 10 Test 293, Run 030 Heating Data MP-1 Configuration
  • TABLE A.31 31-Inch Mach 10 Test 293, Run 031 Heating Data MP-1 Configuration
  • TABLE A.32 31-Inch Mach 10 Test 293, Run 032 Heating Data MP-1 Configuration
  • TABLE A.33 31-Inch Mach 10 Test 293, Run 033 Heating Data MP-1 Configuration
  • TABLE A.34 31-Inch Mach 10 Test 293, Run 034 Heating Data MP-1 Configuration
  • TABLE A.35 31-Inch Mach 10 Test 293, Run 035 Heating Data MP-1 Configuration
  • TABLE A.36 31-Inch Mach 10 Test 293, Run 036 Heating Data MP-1 Configuration
  • TABLE A.37 31-Inch Mach 10 Test 293, Run 037 Heating Data MP-1 Configuration
  • TABLE A.38 31-Inch Mach 10 Test 293, Run 038 Heating Data MP-1 Configuration
  • TABLE A.39 31-Inch Mach 10 Test 293, Run 039 Heating Data MP-2 Configuration
  • TABLE A.40 31-Inch Mach 10 Test 293, Run 040 Heating Data MP-2 Configuration
  • TABLE A.41 31-Inch Mach 10 Test 293, Run 041 Heating Data MP-2 Configuration
  • TABLE A.42 31-Inch Mach 10 Test 293, Run 042 Heating Data MP-2 Configuration
  • TABLE A.43 31-Inch Mach 10 Test 293, Run 043 Heating Data MP-2 Configuration
  • TABLE A.44 31-Inch Mach 10 Test 307, Run 008 Heating Data MP-1 Configuration
  • TABLE A.45 31-Inch Mach 10 Test 307, Run 009 Heating Data MP-1 Configuration
  • TABLE A.46 31-Inch Mach 10 Test 307, Run 010 Heating Data MP-1 Configuration
  • TABLE A.47 31-Inch Mach 10 Test 307, Run 011 Heating Data MP-1 Configuration
  • TABLE A.48 31-Inch Mach 10 Test 307, Run 012 Heating Data MP-1 Configuration
  • TABLE A.49 31-Inch Mach 10 Test 307, Run 013 Heating Data MP-1 Configuration
  • TABLE A.50: 31-Inch Mach 10 Test 307, Run 014 Heating Data MP-1 Configuration
  • TABLE A.51: 31-Inch Mach 10 Test 307, Run 015 Heating Data MP-1 Configuration
  • TABLE A.52 31-Inch Mach 10 Test 307, Run 016 Heating Data MP-1 Configuration
  • TABLE A.53 31-Inch Mach 10 Test 307, Run 017 Heating Data MP-1 Configuration
  • TABLE A.54 31-Inch Mach 10 Test 307, Run 018 Heating Data MP-1 Configuration
  • TABLE A.55 31-Inch Mach 10 Test 307, Run 019 Heating Data MP-1 Configuration
  • TABLE A.56 31-Inch Mach 10 Test 307, Run 020 Heating Data MP-1 Configuration
  • TABLE A.57 31-Inch Mach 10 Test 307, Run 021 Heating Data MP-1 Configuration
  • TABLE A.58 31-Inch Mach 10 Test 307, Run 022 Heating Data MP-1 Configuration
  • TABLE A.59 31-Inch Mach 10 Test 307, Run 023 Heating Data MP-1 Configuration
  • Figure A-1: 31-Inch Mach 10 Test 293, Run 005, MP-1 Configuration
  • Figure A-2: 31-Inch Mach 10 Test 293, Run 006, MP-1 Configuration
  • Figure A-3: 31-Inch Mach 10 Test 293, Run 007, MP-1 Configuration
  • Figure A-4: 31-Inch Mach 10 Test 293, Run 008, MP-1 Configuration
  • Figure A-5: 31-Inch Mach 10 Test 293, Run 009, MP-1 Configuration
  • Figure A-6: 31-Inch Mach 10 Test 293, Run 010, MP-1 Configuration
  • Figure A-7: 31-Inch Mach 10 Test 293, Run 011, MP-2 Configuration
  • Figure A-8: 31-Inch Mach 10 Test 293, Run 012, MP-2 Configuration
  • Figure A-9: 31-Inch Mach 10 Test 293, Run 013, MP-2 Configuration
  • Figure A-10: 31-Inch Mach 10 Test 293, Run 014, MP-2 Configuration
  • Figure A-11: 31-Inch Mach 10 Test 293, Run 015, MP-2 Configuration
  • Figure A-12: 31-Inch Mach 10 Test 293, Run 016, MP-2 Configuration
  • Figure A-13: 31-Inch Mach 10 Test 293, Run 017, MP-3 Configuration
  • Figure A-14: 31-Inch Mach 10 Test 293, Run 018, MP-3 Configuration
  • Figure A-15: 31-Inch Mach 10 Test 293, Run 019, MP-3 Configuration
  • Figure A-16: 31-Inch Mach 10 Test 293, Run 020, MP-3 Configuration
  • Figure A-17: 31-Inch Mach 10 Test 293, Run 021, MP-3 Configuration
  • Figure A-18: 31-Inch Mach 10 Test 293, Run 022, MP-3 Configuration
  • Figure A-19: 31-Inch Mach 10 Test 293, Run 023, MP-4 Configuration
  • Figure A-20: 31-Inch Mach 10 Test 293, Run 024, MP-4 Configuration
  • Figure A-21: 31-Inch Mach 10 Test 293, Run 025, MP-4 Configuration
  • Figure A-22: 31-Inch Mach 10 Test 293, Run 026, MP-4 Configuration
  • Figure A-23: 31-Inch Mach 10 Test 293, Run 027, MP-4 Configuration
  • Figure A-24: 31-Inch Mach 10 Test 293, Run 028, MP-4 Configuration
  • Figure A-25: 31-Inch Mach 10 Test 293, Run 029, MP-1 Configuration
  • Figure A-26: 31-Inch Mach 10 Test 293, Run 030, MP-1 Configuration
  • Figure A-27: 31-Inch Mach 10 Test 293, Run 027, MP-1 Configuration
  • Figure A-28: 31-Inch Mach 10 Test 293, Run 032, MP-1 Configuration
  • Figure A-29: 31-Inch Mach 10 Test 293, Run 033, MP-1 Configuration
  • Figure A-30: 31-Inch Mach 10 Test 293, Run 034, MP-1 Configuration
  • Figure A-31: 31-Inch Mach 10 Test 293, Run 035, MP-1 Configuration
  • Figure A-32: 31-Inch Mach 10 Test 293, Run 036, MP-1 Configuration
  • Figure A-33: 31-Inch Mach 10 Test 293, Run 037, MP-1 Configuration
  • Figure A-34: 31-Inch Mach 10 Test 293, Run 038, MP-1 Configuration
  • Figure A-35: 31-Inch Mach 10 Test 293, Run 039, MP-2 Configuration
  • Figure A-36: 31-Inch Mach 10 Test 293, Run 040, MP-2 Configuration
  • Figure A-37: 31-Inch Mach 10 Test 293, Run 041, MP-2 Configuration
  • Figure A-38: 31-Inch Mach 10 Test 293, Run 042, MP-2 Configuration
  • Figure A-39: 31-Inch Mach 10 Test 293, Run 043, MP-2 Configuration
  • Figure A-40: 31-Inch Mach 10 Test 307, Run 008, MP-1 Configuration
  • Figure A-41: 31-Inch Mach 10 Test 307, Run 009, MP-1 Configuration
  • Figure A-42: 31-Inch Mach 10 Test 307, Run 010, MP-1 Configuration
  • Figure A-43: 31-Inch Mach 10 Test 307, Run 011, MP-1 Configuration
  • Figure A-44: 31-Inch Mach 10 Test 307, Run 012, MP-1 Configuration
  • Figure A-45: 31-Inch Mach 10 Test 307, Run 013, MP-1 Configuration
  • Figure A-46: 31-Inch Mach 10 Test 307, Run 014, MP-1 Configuration
  • Figure A-47: 31-Inch Mach 10 Test 307, Run 015, MP-1 Configuration
  • Figure A-48: 31-Inch Mach 10 Test 307, Run 016, MP-1 Configuration
  • Figure A-49: 31-Inch Mach 10 Test 307, Run 017, MP-1 Configuration
  • Figure A-50: 31-Inch Mach 10 Test 307, Run 018, MP-1 Configuration
  • Figure A-51: 31-Inch Mach 10 Test 307, Run 019, MP-1 Configuration
  • Figure A-52: 31-Inch Mach 10 Test 307, Run 020, MP-1 Configuration
  • Figure A-53: 31-Inch Mach 10 Test 307, Run 021, MP-1 Configuration
  • Figure A-54: 31-Inch Mach 10 Test 307, Run 022, MP-1 Configuration
  • Figure A-55: 31-Inch Mach 10 Test 307, Run 023, MP-1 Configuration
  • APPENDIX B HYPULSE EXPANSION TUBE DATA
  • APPENDIX B HYPULSE EXPANSION TUBE DATA-continue
  • TABLE B.1 HYPULSE Expansion Tube Run Matrix
  • TABLE B.2 HYPULSE Expansion Tube Flow Conditions
  • TABLE B-3: HYPULSE Run 747 Heating Data MP-1 Configuration
  • TABLE B-4: HYPULSE Run 748 Heating Data MP-1 Configuration
  • TABLE B-5 : HYPULSE Run 749 Heating Data MP-1 Configuration
  • TABLE B-6: HYPULSE Run 750 Heating Data MP-2 Configuration
  • TABLE B-7: HYPULSE Run 751 Heating Data MP-2 Configuration
  • TABLE B-8: HYPULSE Run 752 Heating Data MP-1 Configuration
  • TABLE B-9: HYPULSE Run 753 Heating Data MP-2 Configuration
  • TABLE B-10: HYPULSE Run 754 Heating Data MP-1 Configuration
  • TABLE B-11: HYPULSE Run 755 Heating Data MP-2 Configuration
  • TABLE B-12: HYPULSE Run 756 Heating Data MP-2 Configuration
  • TABLE B-13: HYPULSE Run 757 Heating Data MP-1 Configuration
  • TABLE B-14: HYPULSE Run 783 Heating Data MP-1 (SS) Configuration
  • TABLE B-15: HYPULSE Run 784 Heating Data MP-1 (SS) Configuration
  • TABLE B-16: HYPULSE Run 785 Heating Data MP-1 (SS) Configuration
  • TABLE B-17: HYPULSE Run 786 Heating Data MP-1 (SS) Configuration, CO2 Test Gas
  • TABLE B-18: HYPULSE Run 787 Heating Data MP-2 (SS) Configuration, Air Test Gas
  • TABLE B-19: HYPULSE Run 788 Heating Data MP-2 (SS) Configuration, Air Test Gas
  • TABLE B-20: HYPULSE Run 789 Heating Data MP-2 (SS) Configuration, CO2 Test Gas
  • TABLE B-21: HYPULSE Run 790 Heating Data MP-1 Configuration, Air Test Gas
  • TABLE B-22: HYPULSE Run 791 Heating Data MP-2 Configuration, CO2 Test Gas
  • TABLE B-23:  HYPULSE Run 792 Heating Data MP-2 Configuration, CO2 Test Gas
  • TABLE B-24: HYPULSE Run 793 Heating Data MP-3 Configuration, CO2 Test Gas
  • TABLE B-25: HYPULSE Run 794 Heating Data MP-4 Configuration, CO2 Test Gas
  • TABLE B-26: HYPULSE Run 795 Heating Data MP-1 Configuration, Air Test Gas
  • TABLE B-27: HYPULSE Run 796 Heating Data MP-3 Configuration, CO2 Test Gas
  • TABLE B-28: HYPULSE Run 797 Heating Data MP-4 Configuration, CO2 Test Gas
  • TABLE B-29: HYPULSE Run 903 Heating Data MP-1 (SS) Configuration , CO2 Test Gas
  • TABLE B-30: HYPULSE Run 904 Heating Data MP-1 (SS) Configuration, CO2 Test Gas
  • TABLE B-31: HYPULSE Run 905 Heating Data MP-1 (SS) Configuration, Air Test Gas
  • TABLE B-32: HYPULSE Run 906 Heating DataMP-1 (SS) Configuration, Air Test Gas
  • TABLE B-33: HYPULSE Run 907 Heating Data MP-1 (75%) Configuration, CO2 Test Gas
  • TABLE B-34: HYPULSE Run 908 Heating Data MP-1 (75%) Configuration, CO2 Test Gas
  • TABLE B-35: HYPULSE Run 909 Heating Data MP-1 (88%) Configuration, CO2 Test Gas
  • TABLE B-36: HYPULSE Run 910 Heating Data MP-1 (88%) Configuration, CO2 Test Gas
  • TABLE B-37: HYPULSE Run 911 Heating Data MP-1 (75%) Configuration, Air Test Gas
  • TABLE B-38: HYPULSE Run 912 Heating Data MP-1 (75%) Configuration, Air Test Gas
  • TABLE B-39: HYPULSE Run 913 Heating Data MP-1 (88%) Configuration
  • TABLE B-40: HYPULSE Run 914 Heating Data MP-1 (88%) Configuration
  • Figure B-1: HYPULSE Run 747, MP-1 Configuration, CO Test Gas
  • Figure B-2: HYPULSE Run 748, MP-1 Configuration, CO Test Gas
  • igure B-3: HYPULSE Run 749, MP-1 Configuration, CO Test Gas
  • Figure B-4: HYPULSE Run 750, MP-2 Configuration, CO Test Gas
  • Figure B-5: HYPULSE Run 751, MP-2 Configuration, CO Test Gas
  • Figure b-6: HYPULSE Run 752 MP-1 Configuration, Air Test Gas
  • Figure B-7: HYPULSE Run 753, MP-2 Configuration, Air Test Gas
  • Figure B-8: HYPULSE Run 754, MP-1 Configuration , Air Test Gas
  • Figure B-9: HYPULSE Run 755, MP-2 Configuration, Air Test Gas
  • Figure B-10: HYPULSE Run 756, MP-2 Configuration, CO Test Gas
  • Figure B-11: HYPULSE Run 757, MP-1 Configuration, CO Test Gas
  • Figure B-12: HYPULSE Run 783, MP-1 Configuration, Air Test Gas
  • Figure B-13: HYPULSE Run 784, MP-1 Configuration, Air Test Gas
  • Figure B-14: HYPULSE Run 785, MP-1 Configuration, CO Test Gas
  • Figure B-15: HYPULSE Run 786, MP-1 Configuration, CO Test Gas
  • Figure B-16: HYPULSE Run 787, MP-2 Configuration, Air Test Gas
  • Figure B-17: HYPULSE Run 788, MP-2 Configuration, Air Test Gas
  • Figure B-18: HYPULSE Run 789, MP-2 Configuration, CO Test Gas
  • Figure B-19: HYPULSE Run 790, MP-1 Configuration, Air Test Gas
  • Figure B-20: HYPULSE Run 791, MP-2 Configuration, CO Test Gas
  • Figure B-21: HYPULSE Run 792, MP-2 Configuration, CO Test Gas
  • Figure B-22: HYPULSE Run 793, MP-3 Configuration, CO Test Gas
  • Figure B-23: HYPULSE Run 794, MP-4 Configuration, CO Test Gas
  • Figure B-24: HYPULSE Run 795, MP-1 Configuration, Air Test Gas
  • Figure B-25: HYPULSE Run 796, MP-3 Configuration, CO Test Gas
  • Figure B-26: HYPULSE Run 797, MP-4 Configuration, CO Test Gas
  • Figure B-27: Hypulse Run 903, MP-1 Configuration, CO Test Gas
  • Figure B-28: HYPULSE Run 904, MP-1 Configuration, CO Test Gas
  • Figure B-29: HYPULSE Run 905, MP-1 Configuration, Air Test Gas
  • Figure B-30: HYPULSE Run 906, MP-1 Configuration, Air Test Gas
  • Figure B-31: HYPULSE Run 907, MP-1 (75%) Configuration, CO Test Gas
  • Figure B-32: HYPULSE Run 908, MP-1 (75%) Configuration, CO Test Gas
  • Figure B-33: HYPULSE Run 909, MP-1 (88%) Configuration, CO Test Gas
  • Figure B-34: HYPULSE Run 910, MP-1 (88%) Configuration, CO Test Gas
  • Figure B-35: HYPULSE Run 911, MP-1 (75%) Configuration, Air Test Gas
  • Figure B-36: HYPULSE Run 912, MP-1 (75%) Configuration, Air Test Gas
  • Figure B-37: HYPULSE Run 913, MP-1 (88%) Configuration, Air Test Gas
  • Figure B-38: HYPULSE Run 914, MP-1 (88%) Configuration, Air Test Gas
  • APPENDIX C HEMISPHERE CALIBRATION TEST
  • 31-Inch Mach 10 Air Tunnel Tests
  • 31-Inch Mach 10 Air Tunnel Tests-continue
  • 31-Inch Mach 10 Air Tunnel Tests-continue
  • 31-Inch Mach 10 Air Tunnel Tests-continue
  • 31-Inch Mach 10 Air Tunnel Tests-continue
  • HYPULSE Expansion Tube Tests
  • HYPULSE Expansion Tube Tests-continue
  • TABLE C.1.1 31-Inch Mach 10 Test 307 Flow Conditions
  • TABLE C.1.2a 31-Inch Mach 10 Test 307, Run 002 Heating Data
  • TABLE C.1.3a 31-Inch Mach 10 Test 307, Run 003 Heating Data
  • TABLE C.1.4a 31-Inch Mach 10 Test 307, Run 004 Heating Data
  • TABLE C.1.5b 31-Inch Mach 10 Test 307, Run 005 Heating Data
  • TABLE C.1.6a 31-Inch Mach 10 Test 307, Run 006 Heating Data
  • TABLE C.1.7a 31-Inch Mach 10 Test 307, Run 007 Heating Data
  • TABLE C.2.1 HYPULSE Expansion Tube Flow Conditions
  • TABLE C.2.2 HYPULSE Run 758 Heating Data, He Test Gas
  • TABLE C.2.3 HYPULSE Run 759 Heating Data, He Test Gas
  • TABLE C.2.4 HYPULSE Run 760 Heating Data, Air Test Gas
  • TABLE C.2.5 HYPULSE Run 761 Heating Data, Air Test Gas
  • TABLE C.2.6 HYPULSE Run 762 Heating Data, CO2 Test Gas
  • TABLE C.2.7 HYPULSE Run 763 Heating Data, CO2 Test Gas
  • Figure C.1.1 Comparison of Available Data for Macor Thermal Produc
  • Figure C.1.2 Macor Thermal Conductivity Data from Holometrix
  • Figure C.1.3 Macor Thermal Diffusivity Data from Holometrix
  • Figure C.1.4 Quartz Thermal Conductivity Data from Holometrix
  • Figure C.1.5 Quartz Thermal Diffusivity Data from Holometrix
  • Figure C.1.6 Hemisphere Calibration Test Data
  • Figure C.1.7 Hemisphere Calibration Test Data
  • Figure C.1.8 Hemisphere Calibration Test Data
  • Figure C.1.9 Parabolic Temperature Time-History
  • Figure C.1.10 Correction Factor Derivation
  • Figure C.1.11 Correction Factor Applied to Parabolic Temperature Time-History Data
  • Figure C.1.12 Correction Factor Applied to Real Temperature Time History Data
  • Figure C.2.1 HYPULSE Hemisphere Heating Data, He Tests
  • Figure C.2.2 HYPULSE Hemisphere Heating Data, Air Tests
  • Figure C.2.3 HYPULSE Hemisphere Heating Data, CO2 Tests
  • Figure C.2.4 Hemisphere Stagnation Point Heating vs R-1/2
  • Figure C.2.5 Computed Heating Rates vs Experimental Data, Air Test
  • Figure C.2.6 Computed Heating Rates vs Experimental Data, CO2 Tests
  • EXPERIMENTAL AND COMPUTATIONAL AEROTHERMODYNAMICS OF A MARS ENTRY VEHICLE
  • ABSTRACT
  • BIOGRAPHY
  • ACKNOWLEDGMENTS
  • ACKNOWLEDGMENTS-continue
  • TABLE OF CONTENTS
  • TABLE OF CONTENTS-continue
  • TABLE OF CONTENTS-continue
  • LIST OF TABLES
  • LIST OF TABLES-continue
  • LIST OF TABLES-continue
  • LIST OF TABLES-continue
  • LIST OF TABLES-continue
  • LIST OF FIGURES
  • LIST OF FIGURES-continue
  • LIST OF FIGURES-continue
  • LIST OF FIGURES-continue
  • LIST OF FIGURES-continue
  • LIST OF FIGURES-continue
  • LIST OF FIGURES-continue
  • LIST OF FIGURES-continue
  • LIST OF FIGURES-continue
  • LIST OF FIGURES-continue
  • LIST OF FIGURES-continue
  • LIST OF FIGURES-continue
  • LIST OF FIGURES-continue
  • LIST OF FIGURES-continue
  • LIST OF FIGURES-continue
  • LIST OF FIGURES-continue
  • LIST OF FIGURES-continue
  • LIST OF FIGURES-continue
  • LIST OF SYMBOLS
  • LIST OF SYMBOLS-continue
  • LIST OF SYMBOLS-continue
  • LIST OF SYMBOLS-continue
  • CHAPTER 1 INTRODUCTION
  • AEROBRAKING AND AEROASSISTED ORBIT TRANSFER
  • AEROBRAKING AND MARS EXPLORATION MISSIONS
  • BLUNT-BODY AEROBRAKE WAKE FLOW
  • BLUNT-BODY AEROBRAKE WAKE FLOW-continue
  • DESCRIPTION OF RESEARCH
  • DESCRIPTION OF RESEARCH-continue
  • DESCRIPTION OF RESEARCH-continue
  • Figure 1.3.1 Mars Viking Geometry
  • Figure1.3.2 Mars Pathfinder Geometry
  • Figure 1.4.1 Blunt-Body Wake Flow Structure
  • Figure 1.4.2 Aeroassist Flight Experiment (AFE) Vehicle
  • CHAPTER 2 LITERATURE REVIEW
  • Experimental studies
  • Experimental studies-continue
  • Experimental studies-continue
  • Experimental studies-continue
  • Experimental studies-continue
  • Computational studies
  • Computational studies-continue
  • Computational studies-continue
  • CHAPTER 3 MODEL DESIGN AND INSTRUMENTATION
  • Model Configurations
  • Model Construction
  • Model Construction-continue
  • Model Construction-continue
  • Model Instrumentation
  • Model Instrumentation-continue
  • Model Instrumentation-continue
  • Gage Calibration
  • Gage Calibration-continue
  • Gage Calibration-continue
  • Figure 3.1.1 MP-1 Geometry
  • Figure 3.1.2 MP-1 Model and Sting
  • Figure 3.1.3 Parametric Entry Vehicle configurations
  • Figure 3.1.4 MP-1 and MP-2 Configurations
  • Figure 3.1.5 Scaled Stainless-Steel MP-1 Models
  • Figure 3.2.1 Semi-Infinite Test Time vs. Substrate Thickness
  • Figure 3.3.1 Thin-film Gage Details
  • Figure 3.3.2 Thin-Film Gage Layout on MP-1 Model
  • Figure 3.3.3 Thin Film Gage Layout on 1-in. Radius Hemispheres
  • Figure 3.3.4 Thin Film Gage Layout on 1/4-in., 3/8-in. and 1/2-in. Rad. Hemispheres
  • Figure 3.4.1 Typical Thin-Film Gage Voltage-Temperature Calibration
  • CHAPTER 4 EXPERIMENTAL FACILITIES
  • NASA Langley 31-Inch Mach 10 Air Tunnel
  • Flow Conditions
  • NASA HYPULSE Expansion Tube
  • Facility Description
  • Facility Description-continue
  • Flow Conditions and Test Times
  • Flow Conditions and Test Times-continue
  • Flow Conditions and Test Times-continue
  • Flow Conditions and Test Times-continue
  • Table 4.2.1 Flow Conditions for the NASA Langley 31-Inch Mach 10 Air Tunnel
  • Table 4.3.1 Flow Conditions for the NASA HYPULSE Expansion Tube
  • Figure 4.1.1 NASA Langley 31-Inch Mach 10 Air Tunnel
  • Figure 4.1.2 NASA HYPULSE Expansion Tube
  • Figure 4.2.1 Schematic of NASA Langley 31-Inch Mach 10 Air Tunnel
  • Figure 4.2.2 NASA Langley 31-Inch Mach 10 Air Tunnel Pitot Calibration