Experimental investigation of hypersonic buzz on a delta configuration
Oppertunities in flight/propulsion control coupling (FPCC)
Effect of forebody shape and shielding technique on 2-D supersonic inlet performance
Flutter and gust response analysis of flexible aircraft with active control
Project DAME - tactical instrumented missile simulation testing
A theoretical technique for analyzing aeroelastic stability of bearingless rotors
Aircraft operating environments around high-speed ships
A comprehensive analytical model of rotorcraft aerodynamics and dynamics. Part 2: User's manual
A comprehensive analytical model of rotorcraft aerodynamics and dynamics. Part 3: Program manual
Rotor aerodyanmic in ground effect at low advance ratios
Application of time-domain unsteady aerodynamics to rotary-wing aeroelasticity
A zonal method for modeling 3-D aircraft flow fields with jet plume effects
Stability characteristics of a conical aerospace plane concept
Vibration analysis of composite turbopropellers using a nonlinear beam-type finite-element approach
The effect of airframe aerodynamics on V-22 rotor loads
A quasilinear analysis and design technique for nonlinear flight control system
Vorticity equation solutions for slender wings at high incidence
Time and frequency-domain identification and verification of BO 105 dynamic models
Cell-vertex, multigrid Euler scheme for use with multiblock grids
Validation of mathematical simulations of helicopter vertical response characteristics in hover
Hingeless rotor aeroelastic stability analysis with refined aerodynamic modeling
Blade response calcultaions using three-dimensional aerodynamic modeling
Rotor design optimization using a multidisciplinary approach
Estimation of aircraft inertia characteristics from bifilar pendulum test data
Aeromechanical stability of a bearingless composite rotor in forward flight
X-31A flight flutter test excitation by control surfaces