Hypersonic Laminar-Turbulent Transition Experiment Design: From Wind Tunnel Model Definition to MDOE Approach-Reference-Cited by-同舟云学术

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Hypersonic Laminar-Turbulent Transition Experiment Design: From Wind Tunnel Model Definition to MDOE Approach

Published:2010-01-04 Issue: Volume: Page:
ISSN:
Container-title:48th AIAA Aerospace Sciences Meeting Including the New Horizons Forum and Aerospace Exposition
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Author:

Marino Antonello¹,Fauci Roberto¹,Donelli Raffaele¹,Schettino Antonio¹

Affiliation:

1. Italian Aerospace Research Center (CIRA)

Publisher

American Institute of Aeronautics and Astronautics

Link

http://arc.aiaa.org/doi/pdf/10.2514/6.2010-1112

Reference30 articles.

1. J.D.Anderson.Hypersonic andHigh TemperatureGas Dynamics. AIAA.2000.

2. Steven P. Schneider. Hypersonic laminar-turbulent transition on circular cones and scram-jet forebodies. Progress in AerospaceSciences,40(1-2): 1{50,2004.

3. R.G.Batt & H.H. Legner: A review of roughness induced nosetip transition.AIAA Journal, Vol.21,No 1,January1983,pp7-22.

4. Reda, D.C., Review and Synthesis of Roughness-Dominated Transition Correlations for Reentry applications, Journal of Spacecraft and Rockets,Vol.39, No.2,2002,pp.161-167.

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