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Frequenzabhängigkeit
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Initial Assessment of the Ares I-X Launch Vehicle Upper Stage to Vibroacoustic Flight Environments
Fixed Base Modal Testing Using the NASA GRC Mechanical Vibration Facility
Human Transfer Characteristics in Flight and Ground Simulation for a Roll Tracking Task
Propeller Excitation and Response of 230 000 TDW Tankers
Validation of Force Limited Vibration Testing at NASA Langley Research Center
Exterior Electromagnetic Response of NASA F-106 Aircraft
Method for Determining the Time Delay of the Pitot-Static Tubing System of Aircraft
Sinusoidal Vibration Tests on Development Model of Experiment S-126 for Td-2 Spacecraft
Generation of Two-Dimensional Gust Fields in Subsonic Wind-Tunnels
Integrating Flight Dynamics & Control Analysis and Simulation in Rotorcraft Conceptual Design
Limiting Performance of Nonlinear Systems with Applications to Helicopter Vibration Control Problems
Noise Attenuation Performance Assessment of the Joint Helmet Mounted Cueing System (JHMCS)
Dynamic Loads Analysis of Space Vehicle Systems - Launch and Exit Phase
Experimental Damping Studies Monthly Progress Report, 6 Jul. - 5 Aug. 1965
Structural Dynamic Analysis of Rocket Engine Turbomachinery
Response of an Airframe to Sinusodial Wing Flap Deflection
Vibration Mitigation Analysis of a Seahawk Helicopter Seat Suspension Concept
The Derivation of the Transfer Function of a System from Frequency Response Data
Human Pilot Response During Single- and Multi-Axis Tracking Tasks
Electro-Mechanical Actuator. DC Resonant Link Controller
Ground Vibration Test of an F-16 Airplane with Modified Decoupler Pylons
An Improved Ground Vibration Test Method. Volume I. Research Report
Volume II. Flying Qualities Phase. Chapter 13: Feedback Control Theory
Spacecraft Jitter Attenuation Using Embedded Piezoelectric Actuators
Demonstration of Frequency-Sweep Testing Technique Using a Bell 214-ST Helicopter
Evaluation of Image Amplifier Components of Night, AERIAL Photographic Reconnaissance Systems
Accurate Prediction of Longitudinal Flying Qualities for Landing Aircraft
Hybrid Propulsion for Launch Vehicle Boosters: A Program Status Update
Frequency-Domain Identification of XV-15 Tilt-Rotor Aircraft Dynamics