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Frequenzabhängigkeit
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Validation of Force Limited Vibration Testing at NASA Langley Research Center
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
Dynamic Loads Analysis of Space Vehicle Systems - Launch and Exit Phase
Noise Attenuation Performance Assessment of the Joint Helmet Mounted Cueing System (JHMCS)
Experimental Damping Studies Monthly Progress Report, 6 Jul. - 5 Aug. 1965
Structural Dynamic Analysis of Rocket Engine Turbomachinery