YAV-8B Simulation and Modeling. Volume 1: Aircraft Description and Program Summary
Wing Selection and Dynamic Derivative Estimation of a Tailless UAV
Wind Tunnel Tests of an F-8 Airplane Model Equipped with an Oblique Wing
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
Wind Sensing and Estimation Using Small Fixed-Wing Unmanned Aerial Vehicles: A Survey
Volume 1. Performance Flight Testing. Appendix F. Derivations
Virtual simulation of maneuvering captive tests for a surface vessel
Valuation of freight transportation contracts under uncertainty
Use of Time-Frequency Representations for Interpreting Handling Qualities Flight Test Data
Unsteady aerodynamics of a diamond wing configuration
Unsteady aerodynamics of a diamond wing configuration
Trim Calculation of Tandem Rotor Helicopter Using Simplified Rotor System Mathematical Model
Trigger Mechanism for Obtaining Dynamic Derivatives in Wind Tunnels Using Free-Oscillation Technique
Transonic-Small-Disturbance and Linear Analyses for the Active Aeroelastic Wing Program
Third-Generation Light-Driven Symmetric Molecular Motors
Theoretical damping in roll and rolling effectiveness of slender cruciform wings
Tait–Kirchhoff method for determining rotary and unsteady force derivatives
System Identification for Small, Low-Cost, Fixed-Wing Unmanned Aircraft
Super VC 10 Cruise Drag - a Wind Tunnel Investigation. Part 1 - Experimental Techniques
Supersonic Dynamic-Stability Derivatives of the Space Shuttle Launch Vehicle
Sundstrand Model 876 APU. Part II. Storable Propellant
Stall Recovery of a Morphing Wing via Extended Nonlinear Lifting-Line Theory
Stability of Gliding Flight of a Swallowtail Butterfly
Stability Derivatives of Various Lighter-than-Air Vehicles: A CFD-Based Comparative Study
Stability derivatives for a delta-wing X-31 aircraft validated using wind tunnel test data
Stability and Control of Tactical Missile Systems. Held in Ankara (Turkey) on May 9-12, 1988
Stability and Control Derivative Estimates Obtained from Flight Data for the Beech 99 Aircraft
Special Course on Aerodynamic Characteristics of Controls