A Survey of Factors Affecting Blunt-Leading-Edge Separation for Swept and Semi-Slender Wings-Reference-Cited by-同舟云学术

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A Survey of Factors Affecting Blunt-Leading-Edge Separation for Swept and Semi-Slender Wings

Published:2010-06-28 Issue: Volume: Page:
ISSN:
Container-title:28th AIAA Applied Aerodynamics Conference
language:
Short-container-title:

Author:

Luckring James¹

Affiliation:

1. NASA Langley Research Center

Publisher

American Institute of Aeronautics and Astronautics

Link

http://arc.aiaa.org/doi/pdf/10.2514/6.2010-4820

Reference102 articles.

1. 2WhitcombRT.AStudyoftheZero-LiftDragCharacteristicsofWing-BodyCombinationsNeartheSpeedofSound.NACA RM L52H08, Sep 1952.

2. 3AbbottIA,andvonDoenhoffAE.TheoryofWingSections.Dover,1959.

3. 4HummelD.OntheVortexFormationOveraSlenderWingatLargeIncidence.AGARDCP-247,Paper15,Jan1979.

4. 5PolhamusEC.AConceptoftheVortexLiftofSharp-EdgedDeltaWingsBasedonaLeading-EdgeSuctionAnalogy.NASA TN D-3767, Dec 1966.

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