Experimental Optimization of Leading-Edge Deflection Angles for an SST Configuration at Low Speed-Reference-Cited by-同舟云学术

Experimental Optimization of Leading-Edge Deflection Angles for an SST Configuration at Low Speed

Published:2013-01-05 Issue: Volume: Page:
ISSN:
Container-title:51st AIAA Aerospace Sciences Meeting including the New Horizons Forum and Aerospace Exposition
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Author:

Lei Zhong¹,Kwak Dong-youn²,Rinoie Kenichi³

Affiliation:

1. Tokyo University of Science

2. Japan Aerospace Exploration Agency (JAXA)

3. University of Tokyo

Publisher

American Institute of Aeronautics and Astronautics

Link

http://arc.aiaa.org/doi/pdf/10.2514/6.2013-238

Reference7 articles.

1. Quinto, P. F. and Paulson, J. W. Jr.: Flap Effectiveness on Subsonic Longitudinal Aerodynamic Characteristics of a Modified ArrowWing, NASATM-84582,1983.

2. Coe,P.L.Jr.,andWeston,R.P.:Effects ofWingLeading-EdgeDeflectiononLow-SpeedAerodynamicCharacteristicsof aLow-Aspect-Ratio HiqhlySwept Arrow-WingConfiguration, NASATP-1434,1979.

3. Rao,D.M.:Leading-Edge'VortexFlaps'forEnhancedSubsonicAerodynamicsofSlenderWings,ICASPaperNo.80-13.5,

4. Studies on Vortex Flaps with Rounded Leading Edges for Supersonic Transport Configuration

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