In-Flight Receptivity Experiments on a 30-degree Swept-Wing Using Micron-sized Discrete Roughness Elements-Reference-Cited by-同舟云学术

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In-Flight Receptivity Experiments on a 30-degree Swept-Wing Using Micron-sized Discrete Roughness Elements

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:

Carpenter Andrew¹,Saric William¹,Reed Helen¹

Affiliation:

1. Texas A&M University

Publisher

American Institute of Aeronautics and Astronautics

Link

http://arc.aiaa.org/doi/pdf/10.2514/6.2009-590

Reference34 articles.

1. 1Green,J.E."LaminarFlowControl-BacktotheFuture?"AIAA2008-3738,2008.

2. 2Saric,W.S.,Carrillo,R.B.,Reibert,M.S."Leading-EdgeRoughnessasaTransitionControlMechanism,"AIAA98-0781,1998.

3. 4Reed,H.L.,Saric,W.S."TransitionMechanismsforTransportAircraft,"AIAA2008-3743,2008.

4. STABILITY AND TRANSITION OF THREE-DIMENSIONAL BOUNDARY LAYERS

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