Aerodynamic Loads Identification and Modeling of UCAV Configurations with Control Surfaces Using Prescribed CFD Maneuvers
Author:
Affiliation:
1. U.S. Air Force Academy
Publisher
American Institute of Aeronautics and Astronautics
Link
https://arc.aiaa.org/doi/pdf/10.2514/6.2018-2999
Reference17 articles.
1. Experimental and numerical investigation of flight dynamics of a generic lambda wing configuration
2. Accelerating the Numerical Generation of Aerodynamic Models for Flight Simulation
3. Indicial Methods for the Numerical Calculation of Dynamic Derivatives
4. Forced motions design for aerodynamic identification and modeling of a generic missile configuration
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3. Aerodynamic Loads Identification and Modeling of UCAV Configurations with Control Surfaces Using Prescribed CFD Maneuvers;2018 Applied Aerodynamics Conference;2018-06-24
4. Generation of a Reduced Order Model of an Unmanned Combat Air Vehicle using Indicial Response Functions;2018 Applied Aerodynamics Conference;2018-06-24
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