Cylinder-Induced Hypersonic Transitional Shock Wave Boundary Layer Interactions: Pressure Fluctuations and Thermal Loading-Reference-Cited by-同舟云学术

Cylinder-Induced Hypersonic Transitional Shock Wave Boundary Layer Interactions: Pressure Fluctuations and Thermal Loading

Published:2018-09-15 Issue: Volume: Page:
ISSN:
Container-title:22nd AIAA International Space Planes and Hypersonics Systems and Technologies Conference
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Author:

Leidy Andrew¹,Neel Ian T.¹,Tichenor Nathan R.¹,Bowersox Rodney¹,Schmisseur John D.²

Affiliation:

1. Texas A&M University

2. University of Tennessee, Tullahoma

Publisher

American Institute of Aeronautics and Astronautics

Link

https://arc.aiaa.org/doi/pdf/10.2514/6.2018-5374

Reference29 articles.

1. 50 years of shock wave/boundary layer interaction research - What next?

2. 2Knight, D. and Degrez, G. "Shock Wave Boundary Layer Interactions in High Mach Number Flows - A Critical Survey of Current Numerical Prediction Capabilities,"AdvisoryRept. 319,AGARD, Vol.2, Dec. 1998,pp.1.1-1.35.

3. 4Knight,D.andSchmisseur,J.(Editors),"AssessmentofAerothermodynamicFlightPredictionTools,"ProgressinAerospace Sciences, Vol.48-49, 2012,pp.1-74.

4. Supersonic and hypersonic shock/boundary-layer interaction database

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