Experimental results on a mach 14 waverider with blunt leading edges

Journal of Aircraft

Volumn 34, Issue 3, 1997, Pages 296-303

  Gillum, Michael Joseph ^a,c,d   Lewis, Mark J ^b,d,e  

^a NAVAL SURFACE WARFARE CENTER   (United States)

^b UNIVERSITY OF MARYLAND   (United States)

^c Re entry Systems Branch   (United States)

^d AIAA   (United States)

^e Department of Aerospace Engineering ^*

Author keywords

[No Author keywords available]

Indexed keywords

COMPUTATIONAL FLUID DYNAMICS; DRAG; FLOW OF FLUIDS; HYPERSONIC AERODYNAMICS; LIFT; REYNOLDS NUMBER; SHOCK WAVES; VISCOSITY OF GASES; WIND TUNNELS;

BLUNT LEADING EDGES; CONICAL SHOCK; FLOW SPILLAGE; HYPERSONIC WAVERIDERS; MACH NUMBER;

AIRCRAFT;

EID: 0031140464     PISSN: 00218669     EISSN: 15333868     Source Type: Journal    
DOI: 10.2514/2.2198     Document Type: Article

References (21)

1. Burnett, D., and Lewis, M., "A Re-Evaluation of the Waverider Design Process," AIAA Paper 93-0404, Jan. 1993.
2. Takashima, N., and Lewis, M., "Navier Stokes Computation of Hypersonic Viscous Optimized Waveriders," Journal of Spacecraft and Rockets, Vol. 31, No. 3, 1994, pp. 383-391.
3. Cockrell, C. E., Jr., "Interpretation of Waverider Performance Data Using Computational Fluid Dynamics," Journal of Aircraft, Vol. 31, No. 5, 1994, pp. 1095-1100.
4. He, X., and Rasmussen, M. L., "Computational Analysis of OffDesign Waveriders," Journal of Aircraft, Vol. 31, No. 2, 1994, pp. 345-351.
5. He, X., and Rasmussen, M. L., "Nonslender Waveriders," Journal of Aircraft, Vol. 31, No. 1, 1994, pp. 125-131.
6. Vanmol, D. O., Lewis, M., and Anderson, J. D., Jr., "MAXWARP 2.0: Maryland Axisymmetric Waverider Program," Dept. of Aerospace Engineering, UMAERO 92-04, Univ. of Maryland, College Park, MD, 1992.
7. Tincher, D. J., and Burnett, D., "A Hypersonic Waverider Right Test Vehicle: The Next Logical Step," AIAA Paper 92-0308, Jan. 1992.
8. Berry, C., Kammeyer, M., Larach, E., and Burnett, D., "Experiences in Fabrication of a Waverider Model for Wind Tunnel Testing," AIAA Paper 93-0510, Jan. 1993.
9. Kammeyer, M. E., and Gillum, M. J., "Design Validation Tests on a Realistic Hypersonic Waverider at Mach 10, 14, and 16.5 in the Naval Surface Warfare Center Hypervelocity Wind Tunnel No. 9," U.S. Naval Surface Warfare Center, Dahlgren Div., TR-93/198, Silver Spring, MD, May 5, 1994.
10. Ragsdale, W., and Boyd, C., Hypervelocity Wind Tunnel 9 Facility Handbook, 3rd ed., U.S. Naval Surface Warfare Center, Dahlgren Div., TR91-616, Silver Spring, MD, July 26, 1993.
11. Liu, T., Campbell, B., and Sullivan, J. P., "Remote Surface Temperature and Heat Transfer Mapping for a Waverider Model at Mach 10 Using Fluorescent Paint," AIAA Paper 94-2484, June 1994.
12. Gillum, M. J., Kammeyer, M. E., and Bumett, D., "Wind Tunnel Results for a Mach 14 Waverider," AIAA Paper 94-0384, Jan. 1994.
13. "Measurement Uncertainty," Performance Test Codes, Vol. 19.1, American National Standards Inst./American Society of Mechanical Engineers, New York, 1985.
14. Coleman, H., and Steele, G., Experimentation and Uncertainty Analysis for Engineers, Wiley, New York, 1989.
15. Hedlund, E. R., and Kammeyer, M. E., "Aerodynamic and Aerothermal Instrumentation: Measurement Uncertainty in the NSWC Hypervelocity Wind Tunnel #9," AIAA Paper 96-2210, June 1996.
16. Gillum, M. J., Kammeyer, M. E., and Burnett, D., "Details of a Mach 14 Waverider Wind Tunnel Test," AIAA Paper 94-2476, June 1994.
17. Collinbourne, J. R., and Peckham, D. H. "The Lift and Drag Characteristics of Caret Wings at Mach Numbers Between 5 and 10," Ministry of Technology, Aeronautical Research Council Current Papers, 930, London, Feb. 1966.
18. Squire, L. C., "Flow Regimes over Delta Wings at Supersonic and Hypersonic Speeds," Aeronautical Quarterly, Vol. 27, No. 1, 1976, pp. 1-14.
19. Blosser, M. L., Blankson, I. M., Schwoerke, S., Brunson, D., and Hagseth, P., "Wing Leading-Edge Design Concepts for Airbreathing Hypersonic Waveriders," Journal of Aircraft, Vol. 32, No. 2, 1995, pp. 307-313.
20. White, F. M., "Hypersonic Laminar Viscous Interactions on Inclined Flat Plates," ARS Journal, Vol. 32, No. 5, 1962, pp. 780, 781.
21. Lewis, M. J., and Takashima, N., "Engine/Airframe Integration for Waverider Cruise Vehicles," AIAA Paper 93-0404, Jan. 1993.