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Flugmechanik
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X-33 Computational Aeroheating/Aerodynamic Predictions and Comparisons With Experimental Data
X-33 Attitude Control System Design for Ascent, Transition, and Entry Flight Regimes
X-33 Aerodynamic and Aeroheating Computations for Wind Tunnel and Flight Conditions
X-31 Tactical Utility - Initial Results
X-31 post-stall envelope expansion and tactical utility testing
X-31 Post-Stall Envelope Expansion and Tactical Utility Testing
X-31A System Identification Applied to Post-Stall Flight - Aerodynamics & Thrust Vectoring
X-31A System Identification Applied to Post-Stall Flight: Aerodynamics and Thrust Vectoring
X-31 - A Program Overview and Flight Test Status
X-31A High Angle of Attack and Initial Post Stall Flight Testing
X-31A flight flutter test excitation by control surfaces