Numerical Simulations of the F-16XL at Flight-Test Conditions Using Delayed Detached-Eddy Simulation-Reference-Cited by-同舟云学术

Numerical Simulations of the F-16XL at Flight-Test Conditions Using Delayed Detached-Eddy Simulation

Published:2017-11 Issue:6 Volume:54 Page:2077-2099
ISSN:0021-8669
Container-title:Journal of Aircraft
language:en
Short-container-title:Journal of Aircraft

Author:

Lofthouse Andrew J.¹,Cummings Russell M.¹

Affiliation:

1. U.S. Air Force Academy, Colorado 80840

Publisher

American Institute of Aeronautics and Astronautics (AIAA)

Subject

Aerospace Engineering

Link

https://arc.aiaa.org/doi/pdf/10.2514/1.C034045

Reference19 articles.

1. Overview of the Cranked-Arrow Wing Aerodynamics Project International

2. LamarJ.ObaraC.FisherB.FisherD. “Flight, Wind-Tunnel, and Computational Fluid Dynamics Comparison for Cranked Arrow Wing (F-16XL-1) at Subsonic and Transonic Speeds,” NASA TP-2001-210629, 2001.

3. Review of Cranked-Arrow Wing Aerodynamics Project: Its International Aeronautical Community Role

4. F-16XL Unsteady Simulations for the CAWAPI Facet of RTO Task Group AVT-113

5. BertinJ. J.CummingsR. M., Aerodynamics for Engineers, Pearson, Upper Saddle River, NJ, 2014, pp. 404–414.

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