Drag reduction of supersonic cavities via mass injection with applications to scramjets

35th Aerospace Sciences Meeting and Exhibit

Volumn , Issue , 1997, Pages

  Quinn, Jason E ^a   Cutler, Andrew D ^a   Northam, G Burton ^b  

^a GEORGE WASHINGTON UNIVERSITY   (United States)

^b NASA LANGLEY RESEARCH CENTER   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

AEROSPACE ENGINEERING; DUCTS;

COLD FLOW EXPERIMENTS; DIRECT AND INDIRECT MEASUREMENTS; FOCUSING SCHLIEREN; HEIGHT RATIO; MASS INJECTION; RECOMPRESSION; STATIC PRESSURE MEASUREMENTS; SUPERSONIC CAVITY;

DRAG;

EID: 84982318876     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: None     Document Type: Conference Paper

References (15)

1. ‘Stouffer, S. D., "The Effect of Flow Structure on the Combustion and Heat Transfer in a Scramjet Combustor," Ph.D. Dissertation, VPI, Blacksburg, VA, Oct. 14,1995.
2. Komerath, N. M., Ahuja, K. K. and Chambers, F. W., "Prediction and Measurement of Flows Over Cavities - A Survey," AIAA Paper 87-0166, Jan. 1987.
3. Chapman, D. R., "A Theoretical Analysis of Heat Transfer in Regions of Separated Flow," NACA TN-3792, Oct. 1956.
4. Charwat, A. F. and Redekopp, L., "Effect of Mass Addition on the Heat Transfer to a Cavity in Supersonic Flow," Int. J. Heat Mass Transfer, Vol. 11, 1968, pp. 787-804.
5. Vinogradov, V., Grachev, V., Petrov, M. and Sheechman, J., "Experimental Investigation of 2-D Dual Mode Scramjet with Hydrogen Fuel at Mach 4…6," AIAA Paper 90-5269, Oct. 1990.
6. Castiglone, L. A., Northam, G. B., Baker, N. R. and Roe, L. A., "Effect of Cavity Injection on Wall Drag in a Supersonic Flow with Reflecting Shocks," JANNAF Combustion Meeting, 1996.
7. Charwat, A. F., Roos, J. N., Dewey, F. C. and Hitz, J. A., "An Investigation of Separated Flows - Part I: The Pressure Field," Journal of the Aerospace Sciences, Vol. 28, № 6, June 1961, pp. 457-470.
8. Wilcox, F. J., "Experimental Investigation of Porous-Floor Effects on Cavity Flow Fields at Supersonic Speeds," NASA TP-3032, Nov. 1990.
9. Blair, A. B. Jr., and Stallings, R. L. Jr., "Supersonic Axial-Force Characteristics of a Rectangular-Box Cavity with Various Length-to-Depth Ratios in a Flat Plate," NASA TM-87659, March 1986
10. Korte, J. J., Kumar, A., Singh, D. J. and White, J. A., "CAN-DO, CFD-Based Aerodynamic Nozzle Design & Optimization Program for Supersonic/Hypersonic Wind Tunnels," AIAA-92-4009, July 1992.
11. ‘Weinstein, L. M., "Large-Field High-Brightness Focusing Schlieren System," AIAA Journal, Vol. 31, № 7, July 1993, pp. 1250-1255.
12. White, F. M. and Christoph, G. H., "A Simple Theory for the Two-Dimensional Compressible Turbulent Boundary Layer," ASME Journal of Basic Engineering, Sept. 1972, p. 636-642.
13. Baysal, O. and Srinivasan, S., "Unsteady Viscous Calculations of Supersonic Flows Past Deep and Shallow Three-Dimensional Cavities," AIAA-88-0101, Jan. 1988.
14. Charwat, A. F., "Separation of a Supersonic Accelerated Flow over Notches," AIAA Journal, Vol. 9, № 8, Aug. 1971, p. 1656-1657.
15. Quinn, J. E., "Drag Reduction of Supersonic Cavities via Mass Injection with Applications to Scramjets," M.S. Thesis, The George Washington University, JIAFS, Hampton, VA, Expected: June 1997.