Hypersonic boundary layer transition - Application to high speed vehicle design

Collection of Technical Papers - 45th AIAA Aerospace Sciences Meeting

Volumn 6, Issue , 2007, Pages 3792-3803

  Lau, Kei Y ^a,b  

^a BOEING COMPANY   (United States)

^b AIAA   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

AEROSPACE VEHICLES; FLIGHT DYNAMICS; HYPERSONIC FLOW; MACH NUMBER; PHASE TRANSITIONS; REYNOLDS NUMBER; STRUCTURAL DESIGN;

AIRBREATHING HYPERSONIC CONFIGURATIONS; BOUNDARY LAYER TRANSITION; VEHICLE DESIGN;

BOUNDARY LAYERS;

EID: 34250836976     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: 10.2514/6.2007-310     Document Type: Conference Paper

References (15)

1. Lau, K. Y. and Cosner, R. R. "Generic Technology Option #2-Final Report; Volume IV-Blended Wing-Body Aerothermal Model and Test Program". Technical report, McDonnell Douglas Corporation, July 1 1988.
2. Thompson, R. A. and Gnoffo, P. A. "Application of the LAURA Code for Slender-Vehicle Aerothermodynamics". AIAA Paper 90-1714, June 1990.
3. Beckwith, I. E., Chen, F.-J. & Creel, Jr. T. R. "Design requirements for the NASA Langley supersonic low-disturbance wind tunnel", AIAA Paper 86-0763CP, 1986.
4. K. Y. Lau and C. N. Vaporean, Parametric Boundary Layer Transition Study for NASP-like Configuration Using Linear Stability Analyses, National Aerospace Plane Mid-term Technology Review, Monterey CA, April 1992, paper number 283.
5. Malik, M. R., Zang, T., Bushnell, D. "Boundary layer transition in hypersonic. Flows", AIAA Paper 90-5232, (1990).
6. L. M. Mack, "Boundary Layer Linear Stability Theory", in Special Course on Stability and Transition of Laminar Flow, pp. 3/1-3/81, AGARD Report 709, (1984)
7. S. Schwoerke, "Quiet Tunnel Results and Analysis for Various Forebody Shapes at Mach 3.5", in Proceeding of 1993 NASP Mid-term Technology Review, paper no. 158, Monterey, CA, (April 13-16, 1993).
8. NASP Phase II-D Final Report, Section 2.5.4.1, Report Number X30NP94006A, Dec. 1994.
9. Berry, S.A., and Daryabeigi, K., "Preliminary Analysis of Boundary Layer Transition on X-43A Flight 2", 2004 JANNAF Propulsion Meeting, May 10-13, 2004.
10. R.L. Wright and E. V. Zoby, "Flight boundary layer transition measurements on a slender cone at Math 20," AIAA Paper, No. 77-719 (1977).
11. Mujeeb R. Malik, "Hypersonic Flight Transition Data Analysis Using Parabolized Stability Equations with Chemistry Effects", Journal or Spacecraft and Rockets, Vol. 40, No. 3, May-June 2003.
12. Kimmel, R.L., Klein, M.A., and Schwoerke, S.N., "Three-Dimensional Hypersonic Laminar boundary-Layer Computations for Transition Experiment Design", Journal of Spacecraft and Rockets, vol. 34, No. 4, p. 409, July-August 1997.
13. J. Hunt and E. A. Eiswirth, NASA Dual Fuel Airbreathing Hypersonic Vehicle Study, AIAA 7th International Space Planes Conference, Norfolk VA, November 1996, AIAA paper 96-4591.
14. Berry SA, Auslender AH, Dilley AD, and Calleja JF., "Hypersonic Boundary Layer trip Development for Hyper-X". Journal of Spacecaft amd. Rockets, vol. 38, No. 6, pp. 853-864, 2001
15. Berry, S.A., Daryabeigi, K., Auslender, A and Bittner, R., "Boundary Layer Transition on X-43A Flight 2", 2004 JANNAF Propulsion Meeting, June 11-16, 2005.