Prediction of the Flow around the X-31 Aircraft using two different CFD methods
Author:
Affiliation:
1. German Aerospace Center (DLR)
2. National Aerospace Laboratory (NLR)
3. German-Dutch Wind Tunnels
4. Hamburg University of Applied Sciences
Publisher
American Institute of Aeronautics and Astronautics
Link
http://arc.aiaa.org/doi/pdf/10.2514/6.2010-4692
Reference28 articles.
1. Numerical Simulation of Maneuvering Aircraft by Aerodynamic, Flight Mechanics and Structural Mechanics Coupling
2. Experimental and numerical aspects of simulating unsteady flows around the X-31 configuration
3. Ground-Based Simulation of Complex Maneuvers of a Delta-Wing Aircraft
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