Transition Delay in Hypervelocity Boundary Layers by Means of CO2/Acoustic Instability Interactions-Reference-Cited by-同舟云学术

Transition Delay in Hypervelocity Boundary Layers by Means of CO2/Acoustic Instability Interactions

Published:2009-01-05 Issue: Volume: Page:
ISSN:
Container-title:47th AIAA Aerospace Sciences Meeting including The New Horizons Forum and Aerospace Exposition
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Author:

Leyva Ivett¹,Laurence Stuart²,Beierholm Amy²,Hornung Hans²,Wagnild Ross³,Candler Graham³

Affiliation:

1. Air Force Research Laboratory

2. Caltech

3. University of Minnesota

Publisher

American Institute of Aeronautics and Astronautics

Link

http://arc.aiaa.org/doi/pdf/10.2514/6.2009-1287

Reference28 articles.

1. Anderson Jr., J.D.,Hypersonic and High Temperature Gas Dynamics, McGraw-Hill 1989.

2. Heisner, W.H., Pratt, D.T."Hypersonic AirbreathingPropulsion,"AIAA Education Series, 1994. StagnationConditions FreestreamConditions Pressure (MPa) 58.5 Density kg/m30.06032 Temperature (K) 6305.3 Temperature (K) 1564 Enthalpy (MJ/kg) 10.47 Velocity (m/s) 4080 WallTemperature (K) 293 Minf 5.1

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