High-Reynolds Number Circulation Control Testing in the National Transonic Facility (invited)-Reference-Cited by-同舟云学术

High-Reynolds Number Circulation Control Testing in the National Transonic Facility (invited)

Published:2012-01-09 Issue: Volume: Page:
ISSN:
Container-title:50th AIAA Aerospace Sciences Meeting including the New Horizons Forum and Aerospace Exposition
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Author:

Milholen William¹,Jones Gregory¹,Chan David¹

Affiliation:

1. NASA Langley Research Center

Publisher

American Institute of Aeronautics and Astronautics

Link

http://arc.aiaa.org/doi/pdf/10.2514/6.2012-103

Reference20 articles.

1. Zeune,C.H."EnablingSpeedAgilityfortheAirForce",AIAAPaper2010-349,January2010.

2. Collins,S.W.,Westra,B.W.,Lin,J.C.,Jones,G.S.,andZeune,C.H."WindTunnelTesting of PoweredLift,All-WingSTOLModel,"RAeS-566-5A3,presentedatthe2008International PoweredLiftConference,London,UK,July2008.

3. Jones,G.S.,Joslin,R.D."Proceedingsofthe2004NASA/ONRCirculationControl Workshop", NASA/CP-2005-213509,June2005.

4. Englar, R. J. "Development of the A-6 Circulation Control Wing Flight Demonstrator Configuration,"DTNSRDC ReportASED-79/01,January,1979.

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