A database of aerothermal measurements in hypersonic flow in "building block" experiments for CFD validation

41st Aerospace Sciences Meeting and Exhibit

Volumn , Issue , 2003, Pages

  Holden, M S ^a   Wadhams, T P ^b  

^a CUBRC   (United States)

^b Veridian Engineering   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

EID: 84894804417     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: None     Document Type: Conference Paper

References (39)

1. Holden, M. S., "Theoretical and Experimental Studies of the Shock Wave-Boundary Layer Interaction on Curved Compression Surfaces, " Paper presented at the ARL Symposium on Viscous Interaction Phenomena in Supersonic and Hypersonic Flow, WPAFB, OH, 1969.
2. Holden, M. S., "Study of Flow Separation in Regions of Shock Wave-Boundary Layer Interaction in Hypersonic Flow, " AIAA Paper No. 78-1169, July 1978.
3. Kuehn, D. M., "Experimental Investigation of the Pressure Rise Required for the Incipient Separation of Turbulent Boundary Layers in Two-Dimensional Supersonic Flow, " NASA Memo 1-21-59A, 1959.
4. Sterrett, J. R. and Emery, J. C., "Experimental Separation Studies of Two-Dimensional Wedges and Curved Surfaces at Mach Numbers of 4. 8 to 6. 2, " NACA TND-1014.
5. Holden, M. S., "Theoretical and Experimental Studies of the Shock Wave-Boundary Layer Interaction on Curved Compression Surfaces, " paper presented at the ARL Symposium on Viscous Interaction Phenomena in Supersonic and Hypersonic Flow, WPAFB, Ohio, 7-8 May 1969.
6. Holden, M. S., "Theoretical and Experimental Studies of Laminar Flow on Separation on Flat Plate-Wedge Compression Surfaces in the Hypersonic Strong Interaction Regime-Final Report, " Calspan Report No. AF-1894-A-2 ARL 67-0112, May 1967.
7. Cheng, H. K., Hall, J. G., Golian, T. C., and Hertzberg, A., "Boundary-Layer Displacement and Leading-Edge Bluntness in High Temperature Hypersonic Flow, " J. Aero/Space Sci., Vol. 28, No. 5, 1961.
8. Holden, M. S., "Boundary-Layer Displacement and Leading Edge Bluntness Effects on Attached and Separated Laminar Boundary Layers in a Compression Corner, Part II: 'Experimental Study', " AIAA J. Vol. 9, No. 1, pp. 84-93, January 1971.
9. Holden, M. S., Wadhams, T. P., and Candler, G. V., "Measurements in Regions of Low Density Laminar Shock Wave/Boundary Layer Interaction in Hypersonic Flows and Comparison with Predictions, " AIAA Paper 2003-1131, presented at 41st AIAA Aerospace Sciences Meeting and Exhibit, Reno, NV, 6-9 January 2003.
10. Holden, Michael S., Wadhams, Timothy P., Harvey, John K., and Candler, Graham V., "Comparisons between DSMC and Navier-Stokes Solutions on Measurements in Regions of Laminar Shock Wave Boundary Layer Interaction in Hypersonic Flows, " AIAA Paper 2002-0435, presented at the 40th AIAA Aerospace Sciences Meeting and Exhibit, Reno, NV, January 14-17, 2002. Reno, 2002.
11. Holden, M. S., Wadhams, T. P., Harvey, J. K., and Candler, G. V., "Comparisons between Experiments and DSMC and Navier-Stokes Computations for Laminar Shock Wave/Boundary Layer Interaction in Hypervelocity Flows, " AIAA Paper 2003-1131, Reno, NV, January 6-9, 2003.
12. Pate, S. R. and Schueler, C. J., "An Investigation of Radiated Aerodynamic Noise Effects on Boundary-Layer Transition in Supersonic and Hypersonic Wind Tunnels, " AIAA Paper No. 68-375, 1968.
13. Holden, M. S., "An Experimental Investigation of Turbulent Boundary Layers at High Mach Number and Reynolds Numbers, " Calspan Report No. AB-5072-A-1, NASA CR-112147, November 1972.
14. Holden, M. S., Bower, D. R. and Chadwick, K. M., "Measurements of Boundary Layer Transition on Cones at Angle of Attack for Mach Numbers from 11 to 13, " AIAA 95-2294, 26th AIAA Fluid Dynamics Conference, San Diego, CA, June 19-22, 1995.
15. Holden, M. S. and Chadwick, K. M., "Studies of Laminar, Transitional and Turbulent Hypersonic Flows Over Curved Compression Surfaces, " AIAA 95-0093, 33rd Aerospace Sciences Meeting and Exhibit, Reno, NV, January 9-12, 1995.
16. Holden, M. S., "Heat Transfer and Pressure Measurements in Transitional and Turbulent Hypersonic Flows Over Curved Compression Surfaces, " AIAA 96-0666, 34th Aerospace Sciences Meeting and Exhibit, Reno, NV, January 15-18, 1996.
17. Holden, Michael S., "Studies of Scramjet Performance in the LENS Facilities, " presented at the Joint-Army-Navy-NASA-Air Force (JANNAF) CS/APS/PSHS Joint Meeting, Monterey, CA, 13-17 November, 2000.
18. Holden, M. S., and Chadwick, K. M., "Experimental Studies of Relaminarization in Highly Expanding Hypersonic Flows, " Report Number 2610-7, Contract F33601-89-D-0045, prepared for University of Dayton Research Institute, July 1994.
19. Holden, M. S. and Kolly, J. M, "Attachment Line Transition Studies on Swept Cylindrical Leading Edges at Mach Numbers from 10 to 12, " AIAA 95-2279, 26th AIAA Fluid Dynamics Conference, San Diego, CA, June 19-22, 1995.
20. Holden, M. S., "Experimental Studies of Laminar, Transitional and Turbulent Hypersonic Flows over Elliptic Cones at Angles of Attack, " presented at the 22nd International Symposium on Shock Waves, Imperial College, London, England, July 18-23, 1999.
21. Holden, M. S., "Shock-Wave Turbulent Boundary Layer Interaction in Hypersonic Flow, " AIAA Paper No. 72-72, Paper presented at the AIAA 10th Aerospace Sciences Meeting, San Diego, CA 17-19 January 1972.
22. Holden, M. S., "Shock Wave-Turbulent Boundary Layer Interaction in Hypersonic Flow, " paper presented at the AIAA 15th Aerospace Sciences Meeting, Los Angeles, California, AIAA Paper No. 77-45, 24-26 January 1977.
23. Settles, G. S., and Perkins, J. J., "Upstream Influence Scaling of 2D and 3D Shock/Turbulent Boundary Layer Interactions at Compression Corners, " AIAA81-0334, 19th Aerospace Sciences Meeting, 1981.
24. Korkegi, R. H., "A Simple Correlation for Incipient Turbulent Boundary-Layer Separation Due to a Skewed Shock Wave, " AIAA Journal, Vol. 11, No. 11, pp. 1578-1579, 1973.
25. Morkovin, M. V., "Instability, Transition to Turbulence and Predictability, " Keynote Address to AGARD Symposium on Laminar-Turbulent Transition, Technical University of Denmark, Copenhagen, Denmark, 1977.
26. Holden, M. S., "Experimental Studies of Quasi-Two-Dimensional and Three-Dimensional Viscous Interaction Regions Induced by Skewed-Shock and Swept-Shock Boundary Layer Interaction, " AIAA Paper 84-1677, AIAA 19th Thermophysics Conference, Snowmass, Colorado, 25-27 June 1984.
27. Holden, M. S., "Studies of the Mean and Unsteady Structure of Turbulent Boundary Layer Separation in Hypersonic Flow, " AIAA-91-1778, Paper presented at the AIAA 22nd Fluid Dynamics, Plasma Dynamics and Lasers Conference, Honolulu, Hawaii, 24-26 June 1991.
28. Holden, M. S., "Studies of Boundary Layer Transition and Surface Roughness Effects in Hypersonic Flow, " Calspan Report No. 6430-A-5, also AFOSR-TR-84-0251, Report covering period 1 November 1978-30 September 1982, October 1983.
29. Holden, M. S., "Studies of Surface Roughness Effects in Hypersonic Flow, " Calspan Report 7018-A-2, Report covering period 19 August 1982-30 June 1983, October 1983.
30. Finson, M. L. and Wu, P. K. S., "Analysis of Rough Wall Turbulent Heating with Application to Blunted Flight Vehicles, " AIAA Paper No. 79-0008, 17th Aerospace Sciences Meeting, 1979.
31. Holden, M. S., Wieting, A. R., Moselle, J. R. and Glass, C., "Studies of Aerothermal Loads Generated in Regions of Shock/Shock Interaction in Hypersonic Flow, " AIAA-88-0477, AIAA 26th Aerospace Sciences Meeting, Reno, Nevada, 11-14 January 1987.
32. Holden, M. S., Rodriguez, K. M. and Nowak, R. J., "Studies of Shock/Shock Interaction on Smooth and Transpiration-Cooled Hemispherical Nosetips in Hypersonic Flow, " AIAA-91-1765, AIAA 22nd Fluid Dynamics, Plasma Dynamics and Lasers Conference, Honolulu, Hawaii, 24-26 June 1991.
33. Holden, Michael, Sweet, Shirley, Kolly, Joseph, and Smolinski, Gregory, "A Review of the Aerothermal Characteristics of Laminar, Transitional and Turbulent Shock/Shock Interaction Regions in Hypersonic Flows, " AIAA 98-0899, 36th Aerospace Sciences Meeting and Exhibit, Reno, NV, January 12-15, 1998.
34. Holden, M. S., Nowak, R. J., Olsen G. C. and Rodriguez, K. M., "Experimental Studies of Shock Wave/Wall Jet Interaction in Hypersonic Flow, " AIAA-90-0607, Paper presented at the AIAA 28th Aerospace Sciences Meeting, Reno, Nevada, 8-11 January 1990.
35. Holden, M. S., Craig, J. E. and Ratliff, A. W., "The LENS Aero-Optical Evaluation Center and Initial Validation Studies, " Presented at 1993 Missile Sciences Conference, Naval Postgraduate School, Monterey, CA, February 22-24, 1993.
36. Holden, M. S., Neumann, R. D., Burke, J. and Rodriguez, K. M., "An Experimental Study of the Effects of Injectant Properties on the Aerothermal Characteristics of Transpiration-Cooled Cones in Hypersonic Flow, " AIAA-90-1487, Paper presented at the AIAA 21st Fluid Dynamics, Plasma Dynamics and Lasers Conference, Seattle, Washington, 18-20 June 1990.
37. Holden, M. S., "Studies of Surface Roughness and Blowing Effects on Hypersonic Turbulent Boundary Layers Over Slender Cones, " AIAA-89-0458, Paper presented at the AIAA 27th Aerospace Sciences Meeting, Reno, Nevada, 9-12 January 1989.
38. Holden, Michael S., "Synthesis of Comparisons between Prediction and Experiment for Sting-Mounted Planetary Probe Configuration in Hypervelocity Flows, " First Europe-U. S. High Speed Flow Field Workshop-Part II. Blunt Cone Test Case, Naples, Italy, November 12-16, 1997.
39. Holden, Michael, "Shock Interaction in Hypersonic Flows, " AIAA Paper 98-2751, presented at the 29th Plasmadynamics and Laser Conference, Albuquerque, NM, June 15-18, 1998.