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X-56A Structural Dynamics Ground Testing Overview and Lessons Learned
Wessex Helicopter/Sonar Dynamics Study Initial Report
Volume II. Flying Qualities Phase. Chapter 13: Feedback Control Theory
Voltage Controlled Monolithic Oscillator Final Report, Jun. 1967 - Mar. 1969
Vibration Mitigation Analysis of a Seahawk Helicopter Seat Suspension Concept
Validation of Force Limited Vibration Testing at NASA Langley Research Center
Two Techniques for Measuring Locomotion Impact Forces during Zero G
The Derivation of the Transfer Function of a System from Frequency Response Data
Structural Dynamic Analysis of Rocket Engine Turbomachinery
Spacecraft Jitter Attenuation Using Embedded Piezoelectric Actuators
Sinusoidal Vibration Tests on Development Model of Experiment S-126 for Td-2 Spacecraft
Simulation Evaluation of Pilot Inputs for Real Time Modeling During Commercial Flight Operations
Role of Modeling and Flight Testing in Rotorcraft Parameter Identification
Response-TO-Noise Studies of Some Aircraft and Spacecraft Structures
Response of an Airframe to Sinusodial Wing Flap Deflection
Propeller Excitation and Response of 230 000 TDW Tankers
Noise Attenuation Performance Assessment of the Joint Helmet Mounted Cueing System (JHMCS)
Nasa-Langley Helicopter Tower Instrumentation Systems
Method for Determining the Time Delay of the Pitot-Static Tubing System of Aircraft
Limiting Performance of Nonlinear Systems with Applications to Helicopter Vibration Control Problems
Integrating Flight Dynamics & Control Analysis and Simulation in Rotorcraft Conceptual Design
Initial Assessment of the Ares I-X Launch Vehicle Upper Stage to Vibroacoustic Flight Environments
Hybrid Propulsion for Launch Vehicle Boosters: A Program Status Update
Human Transfer Characteristics in Flight and Ground Simulation for a Roll Tracking Task
Human Pilot Response During Single- and Multi-Axis Tracking Tasks
Ground Vibration Test of an F-16 Airplane with Modified Decoupler Pylons
Generation of Two-Dimensional Gust Fields in Subsonic Wind-Tunnels
Frequency-Domain Identification of XV-15 Tilt-Rotor Aircraft Dynamics