F-16XL Simulations at Flight Conditions Using Hybrid Near-Body/Offbody Computational Fluid Dynamics-Reference-Cited by-同舟云学术

F-16XL Simulations at Flight Conditions Using Hybrid Near-Body/Offbody Computational Fluid Dynamics

Published:2017-11 Issue:6 Volume:54 Page:2050-2069
ISSN:0021-8669
Container-title:Journal of Aircraft
language:en
Short-container-title:Journal of Aircraft

Author:

Morton Scott A.¹,McDaniel David R.¹

Affiliation:

1. U.S. Department of Defense, Eglin Air Force Base, Florida 32542

Funder

DoD HPCMP

Publisher

American Institute of Aeronautics and Astronautics (AIAA)

Subject

Aerospace Engineering

Link

https://arc.aiaa.org/doi/pdf/10.2514/1.C034095

Reference23 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 Langley Research Center Rept. TP-2001-21062, Hampton, VA, Feb. 2001.

2. LamarJ. E.ObaraC. J. “Review of Cranked-Arrow Wing Aerodynamics Project: Its International Aeronautical Community Role,” AIAA Paper 2007-0487, Jan. 2007.

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

Cited by 10 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. The Impact of Vortex Breakdown on the Longitudinal Flight Behavior of the Scalos Aircraft;AIAA SCITECH 2024 Forum;2024-01-04

2. Separated and vortical flow in aircraft aerodynamics: a CFD perspective;The Aeronautical Journal;2023-06-15

3. Unsteady Vortex Lattice Linearization and Sensitivity Analyses for Control Models in Supersonic Aircraft Design;AIAA SCITECH 2023 Forum;2023-01-19

4. An Integrated Low-Speed Aeroelastic-Flight-Dynamics Framework for Modeling Supersonic Aircraft;AIAA SCITECH 2022 Forum;2022-01-03

5. Low Speed Aerodynamic Modeling for Control-related Considerations in Supersonic Aircraft Design;AIAA AVIATION 2021 FORUM;2021-07-28