Effect of angle of attack on hypersonic boundary-layer stability

AIAA Journal

Volumn 35, Issue 3, 1997, Pages 464-470

  Doggett, Glen P ^a,c   Chokani, Ndaona ^a,c   Wilkinson, Stephen P ^b,d  

^a NORTH CAROLINA STATE UNIVERSITY   (United States)

^b NASA LANGLEY RESEARCH CENTER   (United States)

^c Department of Mechanical Engineering ^*  (United States)

^d Fluid Mechanics Division   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

EID: 0010113810     PISSN: 00011452     EISSN: None     Source Type: Journal    
DOI: 10.2514/3.13527     Document Type: Article

References (5)

1. Stetson, K. F., and Kimmel, R. L., "On Hypersonic Boundary-Layer Stability " AIAA Paper 92-0737, Jan. 1992.
2. Sheetz, N. W., "Free-Flight Boundary Layer Transition Investigations at Hypersonic Speeds" AIAA Paper 65-127, Jan. 1965.
3. Comte-Bellot, G., "Hot-Wire Anemometry," Handbook of Fluid Dynamics, Oxford Univ. Press, New York, 1995.
4. Kegerise, M. A., and Spina, E. F., "A Comparative Study of Constant-Voltage and Constant-Temperature Hot-Wire Anemometers in Supersonic Flow," Proceedings of the Fluids Engineering Division Summer Meeting, Vol. 4, American Society of Mechanical Engineers, New York, 1996, pp. 297-308.
5. Mack, L. M., "Stability of Axisymmetric Boundary Layers on Sharp Cones at Hypersonic Mach Numbers," AIAA Paper 87-1413, June 1987.