Toward Improved CFD Predictions of Slender Airframe Aerodynamics Using the F-16XL Aircraft (CAWAPI-2)-Reference-Cited by-同舟云学术

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Toward Improved CFD Predictions of Slender Airframe Aerodynamics Using the F-16XL Aircraft (CAWAPI-2)

Published:2014-01-10 Issue: Volume: Page:
ISSN:
Container-title:52nd Aerospace Sciences Meeting
language:
Short-container-title:

Author:

Luckring James M.¹,Rizzi Arthur W.²

Affiliation:

1. NASA Langley Research Center

2. Royal Institute of Technology (KTH)

Publisher

American Institute of Aeronautics and Astronautics

Link

http://arc.aiaa.org/doi/pdf/10.2514/6.2014-0419

Reference18 articles.

1. F-16XL flight test program overview

2. F-16XL demonstrates new capabilities in flight test at Edwards Air Force Base

3. 5Anders, Scott G.; and Fischer, Michael C.: F-16XL-2 Supersonic Laminar Flow Control Flight Test Experiment. NASA/TP1999-209683, December 1999

Cited by 5 articles. 订阅此论文施引文献订阅此论文施引文献，注册后可以免费订阅5篇论文的施引文献，订阅后可以查看论文全部施引文献

1. Hybrid Reynolds-Averaged Navier–Stokes/Large-Eddy Simulations of F-16XL in Low-Speed High-Alpha Flight;Journal of Aircraft;2017-11

2. High-Angle-of-Attack F-16XL Flight Simulations at Sub- and Transonic Speeds;Journal of Aircraft;2017-11

3. F-16XL Hybrid Reynolds-Averaged Navier–Stokes/Large-Eddy Simulation on Unstructured Grids;Journal of Aircraft;2017-11

4. USM3D Simulations for the F-16XL Aircraft Configuration;Journal of Aircraft;2017-03

5. Free-Flight High AoA Flows Simulation at Sub- and Transonic Speeds - F-16XL (CAWAPI-3);33rd AIAA Applied Aerodynamics Conference;2015-06-19

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