Application of a Coupling of Flight Mechanics and Aerodynamics to Predict the SHEFEX I Ascent Phase
Preliminary Design of a Mach 6 Configuration Using MDO
Oppertunities in flight/propulsion control coupling (FPCC)
Effects of a spin chute installation on spin characteristics
Development of an integrated propulsion control system
Modelling the aerodynamics of coaxial helicopters - from an isolated rotor to a complete aircraft
Performance improvement with variable rotor span and RPM
Air-bearing facility for the simulation of spin-stabilized satellites
Experimental and numerical aspects of simulating unsteady flows around the X-31 configuration
Equilibrium motion of unbalanced dual-spin spacecraft
Stability characteristics of a conical aerospace plane concept
Compound Helicopter Optimum Design Based on Genetic Algorithm
Stability of hingeless rotor blades in hover with pitch-link flexibility
Flutter and gust response analysis of flexible aircraft with active control
Effect of forebody shape and shielding technique on 2-D supersonic inlet performance
Addressing today's aeromechanic questions by industrial answers
Status of a digital integrated propulsion/flight control system for the YF-12 airplane
A centrifugal force actuated variable span morphing helicopter rotor
A neural approach for fast simulation of flight mechanics
Extended energy management methods for flight performance optimization
Flow control for aircraft performance enhancements - Overview of airbus - University cooperation
Coupled CFD-simulation of a helicopter in free-flight trim
A zonal method for modeling 3-D aircraft flow fields with jet plume effects
Aerodynamic modelling for flight dynamics analysis of conceptual aircraft designs
Nutzung des A340-Simulators für Flugeigenschaftsanalysen
The implementation of an autonomous helicopter testbed
Stability prediction of sling load dynamics using wind tunnel models
Modeling lead-lag dynamics for rotorcraft-pilot-couplings investigation
Numerical methods for the aeromechanical design of flapping wing hovering MAV
Time-Accurate Simulation of Longitudinal Flight Mechanics with Control by CFD/RBD Coupling
Dynamic analysis of flexible supercavitating vehicles using modal based elements
System concept for a rotorcraft vision system to improve cargo handling operations