Numerical Investigations of Vortical Flow on Swept Wings with Round Leading Edges-Reference-Cited by-同舟云学术

Numerical Investigations of Vortical Flow on Swept Wings with Round Leading Edges

Published:2017-03 Issue:2 Volume:54 Page:572-601
ISSN:0021-8669
Container-title:Journal of Aircraft
language:en
Short-container-title:Journal of Aircraft

Author:

Schütte Andreas¹

Affiliation:

1. DLR, German Aerospace Center, D-38108 Braunschweig, Germany

Publisher

American Institute of Aeronautics and Astronautics (AIAA)

Subject

Aerospace Engineering

Link

https://arc.aiaa.org/doi/pdf/10.2514/1.C034057

Reference65 articles.

1. Static and dynamic numerical simulations of a generic UCAV configuration with and without control devices

2. Review of the Second International Vortex Flow Experiment (VFE-2)

3. ChuJ.LuckringJ. M. “Experimental Surface Pressure Data Obtained on 65-Degree Delta Wing Across Reynolds Number and Mach Number Ranges,” NASA TM-4645, Vols. 1–4, 1996.

4. Experimental and CFD Contribution to Understanding Delta Wing Vortical Flow

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