Sub- and Transonic Vortex Breakdown Flight Condition Simulations of the F-16XL Aircraft-Reference-Cited by-同舟云学术

Sub- and Transonic Vortex Breakdown Flight Condition Simulations of the F-16XL Aircraft

Published:2017-03 Issue:2 Volume:54 Page:428-443
ISSN:0021-8669
Container-title:Journal of Aircraft
language:en
Short-container-title:Journal of Aircraft

Author:

Hitzel Stephan¹

Affiliation:

1. Airbus Defence and Space, D-85077 Manching, Germany

Publisher

American Institute of Aeronautics and Astronautics (AIAA)

Subject

Aerospace Engineering

Link

https://arc.aiaa.org/doi/pdf/10.2514/1.C033246

Reference30 articles.

1. HummelD. “On the Vortex Formation over a Slender Wing at Large Angles of Incidence,” AGARD CP-247, Neuilly sur Seine, France, Oct. 1978.

2. WerleH. “Sur L'eclatement Des Tourbillons,” ONERA–The French Aerospace Lab. TN-175, Paris, 1971.

3. WentzW. H.KohlmanD. L. “Wind-Tunnel Investigations of Vortex Breakdown on Slender Sharp-Edged Wings,” NASA CR-98737, 1968.

4. LambourneN. C.BryerD. W. “Bursting of Leading-Edge Vortices—Some Observations and Discussion of the Phenomenon,” Aeronautical Research Council R&M 3282, April 1961.

5. ChuJ.LuckringJ. M. “Experimental Surface Pressure Data Obtained on Delta Wing Across Reynolds Number and Mach Number Ranges,” Sharp, Small, Medium, Large Leading Edge, Vols. 1–4, NASA TM-4645, Feb. 1996.

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