Initial Experiments and Analysis of Vortex Flow on Blunt Edge Delta Wings-Reference-Cited by-同舟云学术

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Initial Experiments and Analysis of Vortex Flow on Blunt Edge Delta Wings

Published:2008-01-07 Issue: Volume: Page:
ISSN:
Container-title:46th AIAA Aerospace Sciences Meeting and Exhibit
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/10.2514/6.2008-378

Reference19 articles.

1. 1WahlsRA. TheNationalTransonicFacility-AResearchRetrospective.AIAAPaper01-0754,January2001.

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1. Wall Modeled Large Eddy Simulation of the VFE-2 Delta Wing;Direct and Large-Eddy Simulation X;2017-10-08

2. Numerical Investigations of Vortical Flow on Swept Wings with Round Leading Edges;Journal of Aircraft;2017-03

3. Wall Modeled Large Eddy Simulation of a Delta Wing with Round Leading Edge;Notes on Numerical Fluid Mechanics and Multidisciplinary Design;2016

4. Vortical flow prediction for the design of a wind tunnel experiment with a pitching lambda wing;CEAS Aeronautical Journal;2014-07-11

5. Numerical simulation of the peculiar subsonic flow-field about the VFE-2 delta wing with rounded leading edge;Aerospace Science and Technology;2013-01

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