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Standsicherheit
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NASA Langley FUN3D Analyses in Support of the 1st AIAA Stability and Control Prediction Workshop
Investigating the Transonic Flutter Boundary of the Benchmark Supercritical Wing
Nonlinear Unsteady Aerodynamic Modeling Using Wind Tunnel and Computational Data
Integrating Flight Dynamics & Control Analysis and Simulation in Rotorcraft Conceptual Design
Need for the United States Army to Possess a Landing Craft with Maneuver Capabilities
Unsteady Aerodynamic Validation Experiences From the Aeroelastic Prediction Workshop
Investigation of Optimal Control Allocation for Gust Load Alleviation in Flight Control
Submarine and Autonomous Vessel Proliferation: Implications for Future Strategic Stability at Sea
Rebalancing Army Civil Affairs: The Key to Military Governance
Establishing Civil Control: Rule of Law Planning in Future Operations
String Stability of Multiple Surface Marine Vessels