Flight-Test Techniques for Quantifying Pitch Rate and Angle-of-Attack Rate Dependencies
Flight Test Techniques for Quantifying Pitch Rate and Angle of Attack Rate Dependencies
Controlling the Dynamic Environment during NOE (Nap of the Earth) Flight
Analysis of the Wind Tunnel Test of a Tilt Rotor Power Force Model
Free-Flight Model Investigation of a Vertical-Attitude VTOL Fighter
Dynamics of Tilting Proprotor Aircraft in Cruise Flight
Stability and Control Derivatives of the T-37B Airplane
Behavior of Very Large Aircraft Disturbed by Wind Shear and Atmospheric Turbulence
Supersonic Dynamic-Stability Derivatives of the Space Shuttle Launch Vehicle
Aerodynamics Model for a Generic Astovl Lift-Fan Aircraft
Flight-Determined Stability and Control Characteristics of the M2-F3 Lifting Body Vehicle
Flight Evaluation of Advanced Control Systems and Displays on a General Aviation Airplane
Super VC 10 Cruise Drag - a Wind Tunnel Investigation. Part 1 - Experimental Techniques
Impulse of Forces and Moments Experienced by a Slender Wing in Unsteady Flow
YAV-8B Simulation and Modeling. Volume 2: Program Listing
Aerodynamic Characteristic of a Swept-Wing Cruise Missile at Mach Numbers from 0.50 to 2.86
External Store Effects on the Stability of Fighter and Interceptor Airplanes
Wind Tunnel Tests of an F-8 Airplane Model Equipped with an Oblique Wing
Glide-Path Stability of an Aircraft under Speed Constraint
YAV-8B Simulation and Modeling. Volume 1: Aircraft Description and Program Summary
Determination of Aircraft Characteristics from Flight Tests
Selected Flight Test Results for Online Learning Neural Network-Based Flight Control System
Effects of Reynolds Number and Frequency Parameter on Control-Surface Buzz at High Subsonic Speeds