Computational and Experimental Investigation of the Aerodynamics of Unconventional W Wings-Reference-Cited by-同舟云学术

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Computational and Experimental Investigation of the Aerodynamics of Unconventional W Wings

Published:2008-01-07 Issue: Volume: Page:
ISSN:
Container-title:46th AIAA Aerospace Sciences Meeting and Exhibit
language:
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Author:

Musaj Mimoza¹,Prince Simon¹,Cheung Chak-Wah¹

Affiliation:

1. City University

Publisher

American Institute of Aeronautics and Astronautics

Link

http://arc.aiaa.org/doi/pdf/10.2514/6.2008-414

Reference19 articles.

1. The Forward Swept Wing - A unique design challenge

2. 4Putnam,T."X-29Flight-ResearchProgram,"NASA-TM-86025,1984.

3. 5Saltzman, E. J., and Hiks, J. W. "In-Flight Lift-Drag Characteristics for a Forward-Swept Wing Aircraft (and Comparisons With ContemporaryAircraft)," NASA-TM-3414,1994.

4. 6Lemme,H.G."Investigation onaNormalSwept-BackWing,aBluntedSweptBackWingandanMWing,"BritishM.O.S (a),Volkenrode,Reports andTranslationsNo.441,1946.

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1. Compact, Efficient Wing Geometries for Micro Aerial Vehicles;Journal of Aircraft;2020-07

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