Program Overview: Vortex Interaction Aerodynamics Relevant to Military Air Vehicle Performance
Author:
Affiliation:
1. NASA Langley Research Center
2. MBDA
3. Airbus Defence and Space GmbH
Publisher
American Institute of Aeronautics and Astronautics
Link
https://arc.aiaa.org/doi/pdf/10.2514/6.2022-0025
Reference36 articles.
1. Enhanced Maneuverability of a Delta-Canard Combat Aircraft by Vortex Flow Control
2. Collaborative study of incipient separation on 53°-swept diamond wing
3. Integrated Computational/Experimental Approach to Unmanned Combat Air Vehicle Stability and Control Estimation
4. Flow Physics Analyses of a Generic Unmanned Combat Aerial Vehicle Configuration
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1. Introduction to AVT-351: Enhanced Computational Performance and Stability & Control Prediction for NATO Military Vehicles;AIAA SCITECH 2023 Forum;2023-01-19
2. The Influence of Modelling in Predictions of Vortex Interactions About a Generic Missile Airframe: RANS;AIAA SCITECH 2022 Forum;2022-01-03
3. Status of Vortex Interaction on Combat Aircraft - Physics Understood, Simulation Tool Demands, Quality & Cost;AIAA SCITECH 2022 Forum;2022-01-03
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