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Stabilität
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keywords:(Stabilität)
Comparison of Acoustic Models and Trajectory Generation Methods for an Acoustically-Aware Aircraft
Comparison of Acoustic Models and Trajectory Generation Methods for an Acoustically-Aware Aircraft
Aerodynamic Parameter Estimation Using Reconstructed Turbulence Measurements
Flutter Analysis of the Transonic Truss-Braced Wing Aircraft Using Transonic Correction
Dynamic Aeroelastic Flight Dynamic Modeling of Mach 0.745 Transonic Truss-Braced Wing
Comparison of Acoustic Models and Trajectory Generation Methods for an Acoustically-Aware Aircraft
Free-flight and free-oscillation techniques for wind-tunnel dynamic-stability testing
Dynamic Modeling from Flight Data with Unknown Time Skews
A Class of Selenocentric Retrograde Orbits With Innovative Applications to Human Lunar Operations
Computed and Experimental Flutter/LCO Onset for the Boeing Truss-Braced Wing Wind-Tunnel Model
Effect of steady rolling on longitudinal and directional stability
Active Flow Control at Low Reynolds Numbers on a NACA 0015 Airfoil
Low Altitude Mapping Orbit Design and Maintenance for the Dawn Discovery Mission at Vesta
A Guide to Forced Oscillation Data Processing and Analysis
Method of calculating the lateral motions of aircraft based on the Laplace transform
Virtual Deformation Control of the X-56A Model with Simulated Fiber Optic Sensors
Effect of product of inertia on lateral stability
A Stratospheric Test Methodology for Characterizing Free-Flight Dynamics of Entry Vehicles
Aerodynamic forces, moments, and stability derivatives for slender bodies of general cross section
Static Aeroelastic Scaling and Analysis of a Sub-Scale Flexible Wing Wind Tunnel Model
Flutter suppression digital control law design and testing for the AFW wind tunnel model
Modal control of an oblique wing aircraft
Pneumatic system structure for circulation control aircraft
An analysis of a nonlinear instability in the implementation of a VTOL control system during hover
Lightning effects on the NASA F-8 digital-fly-by-wire airplane
Spin Tunnel Investigation of a 1/30 Scale Model of the North American A-5A Airplane
Flutter Tests of Some Simple Models at a Mach Number of 7.2 in Helium Flow
Application of Wind Tunnel Free-Flight Technique for Wake Vortex Encounters
Reduction of wing rock amplitudes using leading-edge vortex manipulations
Active control of gust- and interference-induced vibration of tilt-rotor aircraft
Nonlinear simulation of a flexible aircraft in maneuvering flight
The landing flare: An analysis and flight-test investigation
Integrated aeroservoelastic analysis capability with X-29A analytical comparisons