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Stabilität
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keywords:(Stabilität)
Aerodynamic flight control to increase payload capability of future launch vehicles
Aerodynamic Flight Control to Increase Payload Capability of Future Launch Vehicles
Aerodynamic Flight Control to Increase Payload Capability of Future Launch Vehicles
Aerodynamic forces, moments, and stability derivatives for slender bodies of general cross section
Aerodynamic Forces on Motor Vehicles (Citations from the Engineering Index Data Base)
Aerodynamic Interactions Between a 1/6 Scale Helicopter Rotor and a Body of Revolution
Aerodynamic Parameter Estimation for the X-43A (Hyper-X) from Flight Data
Aerodynamic parameters of High-Angle-of attack Research Vehicle (HARV) estimated from flight data
Aerodynamic parameters of the X-31 drop model estimated from flight-data at high angles of attack
Aerodynamic Performance and Stability Coefficients for the XSM-65A Missile
Aerodynamic Properties of Rough Spherical Balloon Wind Sensors
Aerodynamic Research on the Suitability of a Helicopter for Simulating V/STOL Aircraft
Aerodynamics Model for a Generic Astovl Lift-Fan Aircraft
Aerodynamics of a Model of the Hl-10 Flight- Test Vehicle at Mach 0.35 to 1.80
Aerodynamic Stability and Control Characteristics of Tbc Shuttle Booster AR-11981-3
Aerodynamic Stability Characteristics of the APOLLO Command Module
Aerodynamic stability characteristics of the Apollo launch escape vehicle
Aerodynamic Stability Characteristics of the APOLLO Launch Escape Vehicle
Aerodynamic Static Stability and Control Effectiveness of a Parametric Shuttle Launch Configuration
Aerodynamic, structural, and trajectory analysis of ASTRID-1 vehicle
Aerodynamic Test and Analysis of a Slender Generic Missile Configuration
Aerodynamic Tests of an Operational OH-6A Helicopter in the Ames 40 Ft X 80 Ft Wind Tunnel
Aeroelastic Analysis of the Elastic Gimbal Rotor
Aeroelastic Bending Analysis of a Terrier-Tomahawk 9 Sounding Rocket Vehicle
Aeroelastic control of oblique-wing aircraft
Aeroelastic control of oblique-wing aircraft
Aeroelastic response and blade loads of a composite rotor in forward flight
Aeroelastic Response of the Adaptive Compliant Trailing Edge Transtition Section