Hypersonic Boundary Layer Transition - Application to High Speed Vehicle Design

Author:

Lau Kei1

Affiliation:

1. The Boeing Company

Publisher

American Institute of Aeronautics and Astronautics

Reference15 articles.

1. Thompson, R. A. and Gnoffo, P. A. "Application of the LAURA Code for Slender-Vehicle Aerothermodynamics". AIAA Paper 90-1714, June 1990.

2. Design requirements for the NASA Langley supersonic low-disturbance wind tunnel

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1. Effects of Unforced Bounday Layer Transition on the Performance of a Two-Dimensional Hypersonic Inlet;Applied Mechanics and Materials;2013-01

2. Boundary Layer Transition on the LEA Hypersonic Vehicle Forebody;18th AIAA/3AF International Space Planes and Hypersonic Systems and Technologies Conference;2012-09-24

3. The Aerothermal, Thermal and Structural Design Process and Criteria for the HiFIRE-4 Flight Test Vehicle;18th AIAA/3AF International Space Planes and Hypersonic Systems and Technologies Conference;2012-09-24

4. A Favré averaged transition prediction model for hypersonic flows;Science China Technological Sciences;2010-07-15

5. Boundary Layer Transition on a Hypersonic Forebody: Experiments and Calculations;16th AIAA/DLR/DGLR International Space Planes and Hypersonic Systems and Technologies Conference;2009-06-14

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