Oppertunities in flight/propulsion control coupling (FPCC)
Air-bearing facility for the simulation of spin-stabilized satellites
Development of an integrated propulsion control system
Equilibrium motion of unbalanced dual-spin spacecraft
Status of a digital integrated propulsion/flight control system for the YF-12 airplane
Effect of forebody shape and shielding technique on 2-D supersonic inlet performance
Extended energy management methods for flight performance optimization
Stability of hingeless rotor blades in hover with pitch-link flexibility
Flutter and gust response analysis of flexible aircraft with active control
Effects of a spin chute installation on spin characteristics
A zonal method for modeling 3-D aircraft flow fields with jet plume effects
Stability characteristics of a conical aerospace plane concept
X-31A flight flutter test excitation by control surfaces
Aeromechanical stability of a bearingless composite rotor in forward flight
System concept for a rotorcraft vision system to improve cargo handling operations
Experimental aerodynamic and aeroacoustic investigation of a scaled tilt rotor in hover
Parallel computing of helicopter response to turbulence toward real-time implementation
An unsteady airload model with dynamic stall for rotorcraft simulation
Prediction of rotor aeroacustic in forward flight by a lifting surface method
Propulsion/aircraft integration and dynamic performance of hypersonic TSTO-vehicles
An unsteady vortex wake model for maneuvering vehicles
The Dolphin 6075: an helicopter dedicated to flight test research
Improving helicopter flight mechanics models with laser measurements of blade flapping
Aerodynamic design of the NH90 helicopter stabilizer
TEDAS II - High speed data acquisition, storage and distribution
A novel attitude control technique for miniature spacecraft
Dynamic analysis of flexible supercavitating vehicles using modal based elements
Complex configuration meshing - an industrial view and approach
Optimization of asymmetric oblique flying wing configurations under variable constraints
Incorporation of aircraft performance considerations in inverse airfoil design
Higher order staggered coupling schemes to predict the aeroelastic behavior of helicopter rotors
Stability augmentation of helicopter rotor blades using passive damping of shape memory alloys
V-22 low-speed/high rate of descent (HROD) test results