Hypersonic boundary-layer trip development for Hyper-X-Reference-Cited by-同舟云学术

Hypersonic boundary-layer trip development for Hyper-X

Published:2000-08-14 Issue: Volume: Page:
ISSN:
Container-title:18th Applied Aerodynamics Conference
language:
Short-container-title:

Author:

Berry Scott¹,Auslender Aaron¹,Dilley Arthur¹,Calleja John²

Affiliation:

1. NASA, Langley Research Center, Hampton, VA

2. GASL, Inc., Ronkonkoma, NY

Publisher

American Institute of Aeronautics and Astronautics

Link

http://arc.aiaa.org/doi/pdf/10.2514/6.2000-4012

Reference56 articles.

1. Anderson EC, Lewis CH. 1971.Laminar or Turbulent Boundary-LayerFlows of Perfect Gases or Reacting Gas Mixtures in Chemical Equilibrium. NASA CR-1893

2. Bakos R,Calleja J, ErdosJ. 1996a. An Experimental and Computational Study Leading to New Test Capabilities for the HYPULSE Facility with a Detonation Driver. AIAA Paper 96-2193

3. Bakos R,Castrogiovanni A,Calleja J, Nucci L, ErdosJ. 1996b. Expansion of the Scramjet Ground Test Envelope of the HYPULSE Facility.AIAA Paper 96-4506

4. Baldwin BS, Lomax H. 1978. Thin-LayerApproximation and Algebraic Model for Separated Turbulent Flows. AIAA Paper 78-0257

5. Berry SA, DiFulvio M,Kowalkowski MK.2000a. Forced Boundary LayerTransition on X-43 (Hyper-X) inNASA LaRC 31-Inch Mach 10AirTunnel. NASA/TM-2000-210315

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