Enhancements to the FAST-MAC Circulation Control Model and Recent High-Reynolds Number Testing in the National Transonic Facility-Reference-Cited by-同舟云学术

Enhancements to the FAST-MAC Circulation Control Model and Recent High-Reynolds Number Testing in the National Transonic Facility

Published:2013-06-22 Issue: Volume: Page:
ISSN:
Container-title:31st AIAA Applied Aerodynamics Conference
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Author:

Milholen William E.¹,Jones Gregory S.¹,Chan David T.¹,Goodliff Scott¹,Anders Scott¹,Pack Melton LaTunia G.¹,Carter Melissa B.¹,Allan Brian G.¹,Capone Francis²

Affiliation:

1. NASA Langley Research Center

2. Analytical Mechanics Associates, Inc.

Publisher

American Institute of Aeronautics and Astronautics

Link

http://arc.aiaa.org/doi/pdf/10.2514/6.2013-2794

Reference22 articles.

1. Barberie, F.J., Wick, A.T., Hooker, J.R., Zeune, C.H. "Low Speed Powered Lift Testing of a TransonicCruiseEfficientSTOLMilitaryTransport,",AIAA Paper 2013-1099,January 2013.

2. Harrison, N.A., Vassberg, J.C., DeHann, M.A., Gea, L.M. "The Design and Test of a Swept WingUpperSurfaceBlowing(USB) Concept,"AIAA paper 2013-1102,January 2013.

3. 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.

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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