Hybrid Reynolds-Averaged Navier–Stokes/Large-Eddy Simulations of F-16XL in Low-Speed High-Alpha Flight-Reference-Cited by-同舟云学术

Hybrid Reynolds-Averaged Navier–Stokes/Large-Eddy Simulations of F-16XL in Low-Speed High-Alpha Flight

Published:2017-11 Issue:6 Volume:54 Page:2070-2076
ISSN:0021-8669
Container-title:Journal of Aircraft
language:en
Short-container-title:Journal of Aircraft

Author:

Tomac Maximilian¹,Jirasek Adam²,Rizzi Arthur¹

Affiliation:

1. Royal Institute of Technology, 100 44 Stockholm, Sweden

2. Swedish Defence Research Agency, 164 90 Stockholm Sweden

Publisher

American Institute of Aeronautics and Astronautics (AIAA)

Subject

Aerospace Engineering

Link

https://arc.aiaa.org/doi/pdf/10.2514/1.C034283

Reference20 articles.

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

2. Vortex Flows of the F-16XL Configuration - CAWAPI-II Free-Flight Simulations

3. LamarJ. E. “Cranked Arrow Wing (F-16XL-1) Flight Flow Physics with CFD Predictions at Subsonic and Transonic Speeds,” NATO Research and Technology Organization MP-069, Paris, France, 2003, Paper 44.

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

5. Comparison of Measured and Block Structured Simulation Results for the F-16XL Aircraft

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