YAV-8B Simulation and Modeling. Volume 2: Program Listing
YAV-8B Simulation and Modeling. Volume 1: Aircraft Description and Program Summary
Wind Tunnel Test on a 1/4.622 Froude Scale, Hingeless Rotor, Tilt Rotor Model, Volume 4
Wind Tunnel Test on a 1/4.622 Froude Scale, Hingeless Rotor, Tilt Rotor Model, Volume 3
Wind Tunnel Test on a 1/4.622 Froude Scale, Hingeless Rotor, Tilt Rotor Model, Volume 2
Wind Tunnel Test on a 1/4.622 Froude Scale, Hingeless Rotor, Tilt Rotor Model, Volume 1
Volume 1. Performance Flight Testing. Appendix F. Derivations
Transonic-Small-Disturbance and Linear Analyses for the Active Aeroelastic Wing Program
Theoretical damping in roll and rolling effectiveness of slender cruciform wings
Supersonic Dynamic-Stability Derivatives of the Space Shuttle Launch Vehicle
Sundstrand Model 876 APU. Part II. Storable Propellant
Stability and Control of Tactical Missile Systems. Held in Ankara (Turkey) on May 9-12, 1988
Stability and Control Derivatives of the T-37B Airplane
Stability and Control Derivative Estimates Obtained from Flight Data for the Beech 99 Aircraft
Selected Flight Test Results for Online Learning Neural Network-Based Flight Control System
Real-Time Stability and Control Derivative Extraction From F-15 Flight Data
Propulsion Simulator for Magnetically Suspended Wind Tunnel Models
Parameter Estimation Techniques and Application in Aircraft Flight Testing
Optimization of Turbine Engine Cycle Analysis with Analytic Derivatives
Modelling Helicopter Flight Dynamics: Trim and Stability Analysis
Modeling and Identification of Hover Flight Dynamics for NASA’s Mars Helicopter
Missile Motion Sensitivity to Dynamic Stability Derivatives
Mechanism Modeling and Analysis of a Small Unmanned Vehicles Using Vortex Lattice Method
Interactive Aircraft Flight Control and Aeroelastic Stabilization