Performance study of a power law starbody

Journal of Spacecraft and Rockets

Volumn 36, Issue 5, 1999, Pages 646-652

  Sabean, John W ^a   Lewis, Mark J ^a   Mee, David ^b   Paull, Allan ^b  

^a UNIVERSITY OF MARYLAND   (United States)

^b UNIVERSITY OF QUEENSLAND   (Australia)

Author keywords

[No Author keywords available]

Indexed keywords

BODIES OF REVOLUTION; DRAG; NOSE CONES; NUMERICAL ANALYSIS; WIND TUNNELS;

MACH NUMBER; POWER LAW STARBODY; SCALING EFFECTS;

ROCKETS;

EID: 0033360327     PISSN: 00224650     EISSN: None     Source Type: Journal    
DOI: 10.2514/2.3496     Document Type: Article

References (14)

1. Chernyi, G. G., and Gonor, A. L., "Transversal Contour of Minimum Pressure Drag," Theory of Optimum Aerodynamic Shapes, edited by A. Miele, Academic, New York, 1965, pp. 283-295.
2. Vedernikov, Y., Gonor, A., Zubin, M., and Ostapenko, N., "Aerodynamic Characteristics of Star-Shaped Bodies at Mach Numbers M = 3-5," Izvestiya Akademii Nauk SSSR, Mekhanika Zhidkosti i Gaza, No. 4, July-Aug. 1981, pp. 88-93.
3. Zubin, M. A., Lapygin, V., and Ostapenko, N., "Theoretical and Experimental Investigation into the Structure of Supersonic Flow Past Bodies of Star-Shaped Form and Their Aerodynamic Characteristics," Izvestiya Akademii Nauk SSSR, Mekhanika Zhidkosti i Gaza, No. 3, May-June 1982, pp. 34-40.
4. Foster, N., and Dulikravich, G., "Aerodynamic Characteristics of Star-Shaped Bodies at Mach Numbers M = 3-5," Journal ofSpacecraft and Rockets, Vol. 34, No. 1, 1997, pp. 36-42.
5. Sabean, J., and Lewis, M., "A Parametric Study of Star Bodies for Minimum Drag," Proceedings of the 21st International Symposium on Shock Waves, Paper 7998, 1997.
6. GASP Version 3.0, Aerosoft, Inc., Blacksburg, VA, May 1996.
7. O'Neill, M., and Lewis, M., "Optimized Scramjet Integration on a Waverider," Journal of Aircraft, Vol. 29, No. 6, 1992, pp. 1114-1121.
8. Rasmussen, M., Hypersonic Flow, Wiley, New York, 1994, pp. 101-128.
9. Eckert, E., "Laminar and Turbulent Boundary-Layer Flow over Surfaces with Constant Pressure and Temperature," Transactions of the American Society of Mechanical Engineers, Vol. 78, Aug. 1956, p. 590.
10. Sanderson, S., and Simmons, J., "Drag Balances for Hypervelocity Impulse Facilities," AIAA Journal, Vol. 29, No. 12, 1991, pp. 2185-2191.
11. Turtle, S., Mee, D., and Simmons, J., "Drag Measurements at Mach 5 Using a Stress Wave Force Balance," Experiments in Fluids, Vol. 19, No. 5, 1995, pp. 336-341.
12. Paull, A., Stalker, R., and Mee, D., "Experiments on Supersonic Combustion Ramjet Propulsion in a Shock Tunnel," Journal of Fluid Mechanics, Vol. 296, 1995, pp. 159-183.
13. Mee, D., Daniel, W., and Simmons, J., "Three-Component Force Balance for Flows of Millisecond Duration," AIAA Journal, Vol. 34, No. 3, 1996, pp. 590-595.
14. Prost, R., and Goutte, R., "Three-Component Force Balance for Flows of Millisecond Duration," Signal Processing, Vol. 7, No. 3, 1984, pp. 209-230.