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Back TR-02-27 | Up Costal Inlets Research Program | Next TR-05-2 |
- TR-03-6
- Flow Table Study of Cook Inlet, Alaska
- ABSTRACT
- Contents
- Contents cont'd
- List of Figures
- List of Figures cont'd
- List of Figures cont'd
- List of Figures cont'd
- List of Figures cont'd
- List of Figures cont'd
- List of Figures cont'd
- List of Tables
- Conversion Factors, Non-SI to SI Units of
Measurement
- Preface
- Introduction
- Commerce at Port of Anchorage in 2001 (City of
Anchorage Web Site)
- Problem Background
- Turbulent scale effect in geometrically
distorted physical models
- Task 2: Small-area idealized flow model of
Cook Inlet
- Coastal and Hydraulics Laboratory Flow Table
- Figure 3. Side view of CHL flow table
- Figure 5. View of traversing system looking
down through glass bottom
- Idealized Cook Inlet Models
- Figure 6. Area coverage of large-area and
small-area idealized models
- Large-Area Model Description
- Figure 7. Idealized bathymetry in large-area
model
- Figure 8. Cutting large-area model pieces with
router
- Large-Area Model Observations
- Figure 10. Flood flow in large-area idealized
model
- Figure 12. Alaska District engineers observe
dye patterns in large-area idealized model
- Small-Area Model Description
- Small-Area Model Observations
- Figure 14. Cutting small-area model pieces
with router
- Figure 16. Idealized bathymetry in small-area
model
- Figure 17. Small-area idealized model
positioning on flow table
- Conclusions From Idealized Models
- Turbulence Scale Effect in Distored Models
- Geometrically Distorted Models
- Turbulence Similitude in Geometrically
Distorted Models
- Turbulence Similitude in Geometrically
Distorted Models cont'd
- Turbulence Similitude in Geometrically
Distorted Models cont'd
- Turbulence Similitude in Geometrically
Distorted Models cont'd
- Turbulence Similitude in Geometrically
Distorted Models cont'd
- Anticipated Scale Effects
- Anticipated Scale Effects cont'd
- Flow at Bend
- Flow at Bend cont'd
- Flow at Bend cont'd
- Flow at Bend cont'd
- Flow at Bend cont'd
- Turbulence Scale Effect Experiments
- Case 4: Flow separation at vertical step
- Table 4 Distorted Model Froude Scales
- Case 1: Flow Separation at Vertical Edge -
Free Jet
- Experiment setup
- Figure 20. Experiment setup for Case 1 free
jet flow separation at vertical edge
- Table 5 Distortion Experimental Scale Factors
and Parameters
- Case 1 results
- Figure 21. Velocity field NQ = 1.5, prototype
(Case 1)
- Figure 23. Velocity field NQ = 1.5, distortion
= 4 (Case 1)
- Figure 25. Comparison between prototype and
distortion = 6, NQ = 1.5 (Case 1)
- Figure 27. Crossflow velocity ratios,
distortion = 2,4,6 over prototype (NQ = 1.5, Case 1)
- Case 1 discussion and conclusions
- Case 2 results
- Case 2 discussion and conclusions
- Figure 31. Crossflow velocity ratios,
distortion = 2,4,6 over prototype (NQ = 1.0, Case 2)
- Case 3: Flow separation at sloping edge
- Figure 33. Cross sections showing distortion
for sloping edge tests
- Figure 35. Velocity field at 2/3 d, NQ =1.0,
distortion = 2 (Case 3)
- Figure 37. Velocity field at 2/3 d, NQ =1.0,
distortion = 6 (Case 3)
- Figure 39. Velocity field at 1/3 d, NQ =1.0,
distortion = 2 (Case 3)
- Figure 41. Velocity field at 1/3 d, NQ =1.0,
distortion = 6 (Case 3)
- Figure 42. Velocity field at 2/3 d, NQ =1.0,
prototype vs. distortion = 6 (Case 3)
- Case 3 discussion and conclusions
- Figure 44. Crossflow velocity ratios at 2/3 d,
distortion = 2,4,6 over prototype (No = 1.0, Case 3)
- Figure 46. Crossflow velocity ratios at 1/3 d,
distortion = 2,4,6 over prototype (NQ = 1, Case 3)
- Case 4: Flow Separation at Vertical Step
- Table 7 Distortion in Vertical Step Experiment
- Figure 49. Comparison of horizontal flow
magnitudes in lee of a vertical step
- Conclusions from Turbulence Scale Effects
Experiments
- Impact of Dredging Planform
- Figure 50. Experiment setup for harbor
dredging planform configuration
- Dredge Transition Test Results
- Figure 52. Flow leaving dredged region over
vertical transition
- Figure 54. Flow entering dredged region over
vertical transition
- Figure 56. Photograph of flow entering dredged
region over vertical transition
- Figure 57. Photograph of flow entering dredged
region over sloping transition
- 7 3-D Cook Inlet Model
- Figure 58. Area coverage of 3-D Cook Inlet
model
- Table 10 Scale Ratios for 3-D Model
- Model fabrication
- Figure 60. Router rough-cut of bathymetry
- Figure 61. Router finish cut of bathymetry
- Figure 63. Portion of 3-D model looking
downstream
- Model operation
- Figure 66. 3-D Cook Inlet model installed for
flood flow
- 3-D Model Observations
- Figure 67. Surface flow tracer showing reduced
flow at Port of Anchorage during ebb tide
- Figure 69. Aerial showing approximate flow
separation and entrainment region in lee of Carin Point during ebb tide
- Conclusions from Cook Inlet 3-D Model
- Conclusions from Cook Inlet 3-D Model cont'd
- Summary and Conclusions
- Task 3: Turbulence scale effect in distorted
physical models
- Study Conclusions
- Turbulence scale effects study conclusions
- Turbulence scale effects study conclusions
cont'd
- References
- Appendix A Case 1 - Flow Separation at
Vertical Edge - Free Jet
- Figure A1. Case 1, Q = 1.5 L/sec, prototype
- Figure A3. Case 1, Q = 1.5 L/sec, distortion =
4
- Figure A5. Case 1, Q = 1.5 L/sec, prototype
vs. distortion = 2
- Figure A7. Case 1, Q = 1.5 L/sec, prototype
vs. distortion = 6
- Figure A9. Case 1, Q = 1.5 L/sec, prototype
minus distortion = 4
- Figure A11. Case 1, Q = 1.5 L/sec, ratios
between prototype and distortions 2, 4, and 6
- Figure A13. Case 1, Q = 1.0 L/sec, prototype
- Figure A15. Case 1, Q = 1.0 L/sec, distortion
= 4
- Figure A17: Case 1, Q = 1.0 L/sec, prototype
vs. distortion = 2
- Figure A19. Case 1, Q = 1.0 L/sec, prototype
vs. distortion = 6
- Figure A21. Case 1, Q = 1.0 L/sec, prototype
minus distortion = 4
- Figure A23. Case 1, Q = 1.0 L/sec, ratios
between prototype and distortions 2, 4, and 6
- Figure A25. Case 1, Q = 0.75 L/sec, prototype
- Figure A27. Case 1, Q = 0.75 L/sec, distortion
= 4
- Figure A29. Case 1, Q = 0.75 L/sec, prototype
vs. distortion = 2
- Figure A31. Case 1, Q = 0.75 L/sec, prototype
vs. distortion = 6
- Figure A33. Case 1, Q = 0.75 L/sec, prototype
minus distortion = 4
- Figure A35. Case 1, Q = 0.75 L/sec, ratios
between prototype and distortions 2, 4, and 6
- Appendix B Case 2 - Flow Separation at
Vertical Edge - Constrained Jet
- Figure B1. Case 2, Q = 1.5 L/sec, prototype
- Figure B3. Case 2, Q = 1.5 L/sec, distortion =
4
- Figure B5. Case 2, Q = 1.5 L/sec, prototype
vs. distortion = 2
- Figure B7. Case 2, Q = 1.5 L/sec, prototype
vs. distortion = 6
- Figure B9. Case 2, Q = 1.5 L/sec, prototype
minus distortion = 4
- Figure B11. Case 2, Q = 1.5 L/sec, ratios
between prototype and distortions 2, 4, and 6
- Figure B13. Case 2, Q = 1.0 L/sec, prototype
- Figure B15. Case 2, Q = 1.0 L/sec, distortion
= 4
- Figure B17. Case 2, Q = 1.0 L/sec, prototype
vs. distortion = 2
- Figure B19. Case 2, Q = 1.0 L/sec, prototype
vs. distortion = 6
- Figure B21. Case 2, Q = 1.0 L/sec, prototype
minus distortion = 4
- Figure B23. Case 2, Q = 1.0 L/sec, ratios
between prototype and distortions 2, 4, and 6
- Figure B25. Case 2, Q = 0.75 L/sec, prototype
- Figure B27. Case 2, Q = 0.75 L/sec, distortion
= 4
- Figure B29. Case 2, Q = 0.75 L/sec, prototype
vs. distortion = 2
- Figure B31. Case 2, Q = 0.75 L/sec, prototype
vs. distortion = 6
- Figure B33. Case 2, Q = 0.75 L/sec, prototype
minus distortion = 4
- Figure B35. Case 2, Q = 0.75 L/sec, ratios
between prototype and distortions 2, 4, and 6
- Appendix C Case 3 - Flow Separation at Sloping
Edge
- Figure C1. Case 3 (1/3 d), Q = 1.5 L/sec,
prototype
- Figure C3. Case 3 (1/3 d), Q = 1.5 L/sec,
distortion = 4
- Figure C5. Case 3 (1/3 d), Q = 1.5 L/sec,
prototype vs. distortion = 2
- Figure C7. Case 3 (1/3 d), Q = 1.5 L/sec,
prototype vs. distortion = 6
- Figure C9. Case 3 (1/3 d), Q = 1.5 L/sec,
prototype minus distortion = 4
- Figure C11. Case 3 (1/3 d), Q = 1.5 L/sec,
ratios between prototype and distortions 2, 4, and 6
- Figure C13. Case 3 (2/3 d), Q = 1.5 L/sec,
prototype
- Figure C15. Case 3 (2/3 d), Q = 1.5 L/sec,
distortion = 4
- Figure C17. Case 3 (2/3 d), Q = 1.5 L/sec,
prototype vs. distortion = 2
- Figure C19. Case 3 (2/3 d), Q = 1.5 L/sec,
prototype vs. distortion = 6
- Figure C21. Case 3 (2/3 d), Q = 1.5 L/sec,
prototype minus distortion = 4
- Figure C23. Case 3 (2/3 d), Q = 1.5 L/sec,
ratios between prototype and distortions 2, 4, and 6
- Figure C25. Case 3 (1/3 d), Q = 1.0 L/sec,
prototype
- Figure C27. Case 3 (1/3 d), Q = 1.0 L/sec,
distortion = 4
- Figure C29. Case 3 (1/3 d), Q = 1.0 L/sec,
prototype vs. distortion = 2
- Figure C31. Case 3 (1/3 d), Q = 1.0 L/sec,
prototype vs. distortion = 6
- Figure C33. Case 3 (1/3 d), Q = 1.0 L/sec,
prototype minus distortion = 4
- Figure C35. Case 3 (1/3 d), Q = 1.0 L/sec,
ratios between prototype and distortions 2, 4, and 6
- Figure C37. Case 3 (2/3 d), Q = 1.0 L/sec,
prototype
- Figure C39. Case 3 (2/3 d), Q = 1.0 L/sec,
distortion = 4
- Figure C41. Case 3 (2/3 d), Q = 1.0 L/sec,
prototype vs. distortion = 2
- Figure C43. Case 3 (2/3 d), Q = 1.0 L/sec,
prototype vs. distortion = 6
- Figure C45. Case 3 (2/3 d), Q = 1.0 L/sec,
prototype minus distortion = 4
- Figure C47. Case 3 (2/3 d), Q = 1.0 L/sec,
ratios between prototype and distortions 2, 4, and 6
- REPORT DOCUMENTATION PAGE
- (Concluded)
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