Computational Fluid Dynamics Predictions of Control-Surface Effects for F-16XL Aircraft-Reference-Cited by-同舟云学术

Computational Fluid Dynamics Predictions of Control-Surface Effects for F-16XL Aircraft

Published:2017-03 Issue:2 Volume:54 Page:395-408
ISSN:0021-8669
Container-title:Journal of Aircraft
language:en
Short-container-title:Journal of Aircraft

Author:

Tomac M.¹,Rizzi A.¹,Jirásek A.²

Affiliation:

1. Royal Institute of Technology, Stockholm, Sweden

2. Swedish Defence Research Agency, FOI, Stockholm, Sweden

Publisher

American Institute of Aeronautics and Astronautics (AIAA)

Subject

Aerospace Engineering

Link

https://arc.aiaa.org/doi/pdf/10.2514/1.C033260

Reference17 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. Overview of the Cranked-Arrow Wing Aerodynamics Project International

3. Lessons Learned from Numerical Simulations of the F-16XL Aircraft at Flight Conditions

4. F16-XL Geometry and Computational Grids Used in Cranked-Arrow Wing Aerodynamics Project International

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

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