Studies of scramjet performance in the LENS facilities

36th AIAA/ASME/SAE/ASEE Joint Propulsion Conference and Exhibit

Volumn , Issue , 2000, Pages

  Holden, Michael S ^a  

^a CUBRC   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

AERODYNAMICS; MACH NUMBER; NASA; PROPULSION; TEST FACILITIES;

ACCURATE MEASUREMENT; CALIBRATION AND VALIDATIONS; DYNAMIC PRESSURES; ENGINE CONFIGURATION; ENGINE PERFORMANCE; EXPERIMENTAL PROGRAM; FLIGHT CONDITIONS; STAGNATION PRESSURES;

ENGINES;

EID: 84895110810     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: None     Document Type: Conference Paper

References (10)

1. Holden, M.S., Chadwick, K.M., and Kolly, J.M., "Hypervelocity Vehicle and Combustion Studies in the LENS Facility," paper presented at the 1995 JANNAF Airbreathing Propulsion Subcommittee Meeting, MacDill Air Force Base, Tampa, FL, December 5-8, 1995.
2. Holden, M.S., "Heat Transfer and Pressure Measurements in Transitional and Turbulent Hypersonic Flows Over Curved Compression Surfaces," Report Number 2610-2, Contract F33601-89-D-0045, prepared for University of Dayton Research Institute, May 1994.
3. Holden, M.S., "Experimental Studies of Transpiration Cooling With Shock Interaction in Hypersonic Flow," Final Report Part B, Grant Number NAG 1-790, prepared for NASA Langley Research Center, May 1994.
4. 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," Report Number 2610- 4, Contract F33601-89-D-0045, prepared for University of Dayton Research Institute, May 1994.
5. Holden, M.S. and Sweet, S. J., "Studies of Transpiration Cooling With Shock Interaction in Hypersonic Flow," AIAA-94-2475, Paper presented at the 18th AIAA Aerospace Ground Testing Conference, Colorado Springs, CO, June 20-23, 1994.
6. Holden, M.S., Kolly, J.M., and Bower, D.R., "Attachment-Line Transition Studies on Swept Cylindrical Leading Edges at Mach Numbers From 10 to 12," Report Number 2610-6, Contract F33601-89-D-0045, prepared for University of Dayton Research Institute, July 1994
7. 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.
8. 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, paper presented at the 26th AIAA Ruid Dynamics Conference in San Diego, CA, June 19-22, 1995.
9. 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, presented at the 36th Aerospace Sciences Meeting and Exhibit, Reno, NV, January 12-15, 1998.
10. Dash, S.M., Perrell, E.R., Hosangadi, A., Ungewitter, R., Cavallo, P.A., Kenzakowski, D.C., Seiner, J., and Holden, M., "Missile Flowfield Modeling Advances and Data Comparisons," paper presented at the 38th Aerospace Sciences Meeting & Exhibit, Reno, NV, AIAA 2000-0940, January 10-13, 2000.