Fin leading-edge sweep effect on shock-shock interaction at Mach 6

Journal of Spacecraft and Rockets

Volumn 34, Issue 4, 1997, Pages 416-425

  Berry, Scott A ^a   Nowak, Robert J ^a,b  

^a NASA LANGLEY RESEARCH CENTER   (United States)

^b AIAA   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

FINS (HEAT EXCHANGE); FLOW INTERACTIONS; HEAT TRANSFER; IMAGE ANALYSIS; REYNOLDS NUMBER; SENSORS; WIND TUNNELS;

FIN LEADING EDGE SWEEP EFFECT; MACH NUMBER; PLANAR INCIDENT SHOCK; SCHLIEREN IMAGES; SHOCK SHOCK INTERACTION;

SHOCK WAVES;

EID: 0031193126     PISSN: 00224650     EISSN: 15336794     Source Type: Journal    
DOI: 10.2514/2.3247     Document Type: Article

References (20)

1. Edney, B., "Anomalous Heat Transfer and Pressure Distributions on Blunt Bodies at Hypersonic Speeds in the Presence of an Impinging Shock," Aeronautical Research Inst. of Sweden, Rept. 115, Feb. 1968.
2. Holden, M., and Kolly, J., "Measurements of Heating in Regions of Shock/Shock Interaction in Hypersonic Flow," AIAA Paper 95-0640, Jan. 1995.
3. Hackett, C. M., and Calleja, J., "Exploratory Study of Heating Due to a Hypersonic, High-Enthalpy Shock/Shock Interaction," AIAA Paper 95-2216, June 1995.
4. Carlson, A. B., and Wilmoth, R. G., "Monte Carlo Simulation of a Near-Continuum Shock-Shock Interaction Problem," Journal of Spacecraft and Rockets, Vol. 31, No. 1, 1994, pp. 25-30.
5. Prabhu, R. K., "An Implementation of a Chemical and Thermal Nonequilibrium Flow Solver on Unstructured Meshes and Application to Blunt Bodies," NASA CR 194967, Aug. 1994.
6. Vemaganti, G. R., "Laminar and Turbulent Flow Computations of Type IV Shock-Shock Interference Aerothermal Loads Using Unstructured Grids," NASA CR 195008, Oct. 1994.
7. Bushnell, D. M., "Interference Heating on a Swept Cylinder in Region of Intersection with a Wedge at Mach Number 8," NASA TN D-3094, Dec. 1965.
8. Bushnell, D. M., "Effects of Shock Impingement and Other Factors on Leading-Edge Heat Transfer," NASA TN D-4543, April 1968.
9. Heirs, R. S., and Loubsky, W. J., "Effects of Shock-Wave Impingement on the Heat Transfer on a Cylindrical Leading Edge," NASA TN D-8859, Feb. 1967.
10. Keyes, J. W., and Hains, F. D., "Analytical and Experimental Studies of Shock Interference Heating in Hypersonic Flow," NASA TN D-7139, May 1973.
11. Singh, D. J., Kumar, A., and Tiwari, S. N., "Three-Dimensional Shock-Shock Interactions on the Scramjet Inlet," AIAA Paper 90-0529, Jan. 1990.
12. Singh, D. J., Kumar, A., and Tiwari, S. N., "Numerical Simulation of Three-Dimensional Shock-Shock Interactions on a Blunt Body," Computational Fluid Dynamics, Vol. 1, Gordon and Breach, New York, 1993, pp. 177-196.
13. Miller, C. G., "Langley Hypersonic Aerodynamic/Aerothermodynamic Testing Capabilities - Present and Future," AIAA Paper 90-1376, June 1990.
14. Micol, J. R., "Hypersonic Aerodynamic/Aerothermodynamic Testing Capabilities at Langley Research Center: Aerothermodynamic Facilities Complex," AIAA Paper 95-2107, June 1995.
15. Miller, C. G., "Comparison of Thin-Film Resistance Heat-Transfer Gages with Thin-Skin Transient Calorimeter Gages in Conventional Hypersonic Wind Tunnels," NASA TM 83197, Dec. 1981.
16. Miller, C. G., Micol, J. R., and Gnoffo, P. A., "Laminar Heat-Transfer Distributions on Biconics at Incidence in Hypersonic-Hypervelocity Flows," NASA TP 2213, 1984.
17. Hollis, B. R., "User's Manual for the One Dimensional Hypersonic Experimental Aero-Thermodynamic (1DHEAT) Data Reduction Code," NASA CR 4691, Aug. 1995.
18. Cook, W. J., and Felderman, E. J., "Reduction of Data from Thin-Film Heat-Transfer Gages: A Concise Numerical Technique," AIAA Journal, Vol. 4, No. 3, 1966, pp. 561, 562.
19. Hollis, B. R., and Perkins, J. N., "High-Enthalpy and Perfect Gas Heating Measurements on a Blunt Cone," Journal of Spacecraft and Rockets, Vol. 33, No. 5, 1996, pp. 628-634.
20. Micol, J. R., "Aerothermodynamic Measurement and Prediction for Modified Orbiter at Mach 6 and 10," Journal of Spacecraft and Rockets, Vol. 32, No. 5, 1995, pp. 737-748.