Initial Assessment of a Variable-Camber Continuous Trailing-Edge Flap System for Drag-Reduction of Non-Flexible Aircraft in Steady-State Cruise Condition-Reference-Cited by-同舟云学术

Initial Assessment of a Variable-Camber Continuous Trailing-Edge Flap System for Drag-Reduction of Non-Flexible Aircraft in Steady-State Cruise Condition

Published:2013-08-15 Issue: Volume: Page:
ISSN:
Container-title:AIAA Infotech@Aerospace (I@A) Conference
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Author:

Ippolito Corey A.¹,Nguyen Nhan T.¹,Totah Joseph¹,Trinh Khanh²,Ting Eric B.²

Affiliation:

1. NASA Ames Research Center

2. Stinger Ghaffarian Technologies, Inc.

Publisher

American Institute of Aeronautics and Astronautics

Link

http://arc.aiaa.org/doi/pdf/10.2514/6.2013-5143

Reference9 articles.

1. 2BoeingReportNo.2012X0015,"DevelopmentofVariableCamberContinuousTrailingEdgeFlapSystem,"October4,2012.

2. 4Nguyen, N., Urnes, J. "Aeroelastic Modeling of Elastically Shaped Aircraft Concept viaWing Shaping Control for Drag Reduction,"AIAAAtmosphericFlight MechanicsConference, AIAA-2012-4642, August2012.

3. 5Jordan, T. L., Langford, W. M., Belcastro, C. M., Foster, J. M., Shah, G. H., Howland, G., and Kidd, R. "Development of a DynamicallyScaledGenericTransportModelTestbedforFlightResearchExperiments,"AUVSIUnmannedUnlimited,Arlington, VA, 2004.

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