Design of a Swept-Wing Laminar Flow Control Flight Experiment for Transonic Aircraft-Reference-Cited by-同舟云学术

Design of a Swept-Wing Laminar Flow Control Flight Experiment for Transonic Aircraft

Published:2010-06-28 Issue: Volume: Page:
ISSN:
Container-title:28th AIAA Applied Aerodynamics Conference
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Author:

Belisle Michael¹,Neale Tyler¹,Reed Helen¹,Saric William¹

Affiliation:

1. Texas A&M University

Publisher

American Institute of Aeronautics and Astronautics

Link

http://arc.aiaa.org/doi/pdf/10.2514/6.2010-4381

Reference23 articles.

1. AVT-151 RTO AVT/VKI Lecture Series,2009

2. Boppe CW.1984.Elementsofcomputationalengine-airframeintegration. AIAA-1984-0117.

3. Chang C. 2003. The Langley stability and transition analysis code (LASTRAC): LST, linear & nonlinear PSE for 2-D, axisymmetric,andinfiniteswept wingboundarylayers. AIAA-2003-0974.

4. ChangC,ChoudhariM. 2005. Boundary-layer receptivityandintegratedtransition prediction. AIAA-2005-0526.

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