Wind Biasing Techniques for Use in Obtaining Load Relief
What Was Learned in Predicting Slender Airframe Aerodynamics with the F16-XL Aircraft
Vortex Wake Geometry of a Model Tilt Rotor in Forward Flight
Vortex Velocity Distributions at Large Downstream Distances
Vortex Induced Characteristics of Missiles in Unsteady Maneuvers
Vortex Flap Technology: A Stability and Control Assessment
Volume II. Flying Qualities Phase. Chapter 14: Flight Control Systems
Volume II. Flying Qualities Phase. Chapter 6: Maneuvering Flight
Volume II. Flying Qualities Phase. Chapter 4: Equations of Motion
Volume II. Flying Qualities Flight Testing Phase. Chapter 10: High Angle of Attack
Volume 1. Performance Phase. Chapter 11. Cruise Performance Theory
VLA Missile Development and High Angle of Attack Behavior
Vista/F-16 Multi-Axis Thrust Vectoring (MATV) Control Law Design and Evaluation
Viscous Drag Calculations for Ship Hull Geometry
Verification of the Production Safe Flight Instrument Corporation OV/RV-1D Stall Warning System
Validation Study of the V/STOL Aerodynamics and Stability and Control Manual