Numerical Simulation and Reduced-Order Aerodynamic Modeling of a Lambda Wing Configuration
Author:
Affiliation:
1. High Performance Computing Research Center, U.S. Air Force Academy, Colorado 80840
2. Defence Science and Technology Group, Melbourne, Victoria 3207, Australia
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
https://arc.aiaa.org/doi/pdf/10.2514/1.C033776
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5. Conceptual Design and Aerodynamic Analyses of a Generic UCAV Configuration
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