Vorticity equation solutions for slender wings at high incidence
A zonal method for modeling 3-D aircraft flow fields with jet plume effects
Vortraege des DFVLR-Kolloquiums am 8. Mai 1973 im Forschungszentrum Porz-Wahn
Flow control for aircraft performance enhancements - Overview of airbus - University cooperation
Performance analysis of the slowed-rotor compound helicopter configuration
Stability and control analysis of the slowed-rotor compound helicopter configuration
A severity analysis for rotorcraft encounters with vortex wakes
Analysis of partial wing damage on flying-wing unmanned air vehicle
System identification modeling of a small-scale unmanned rotorcraft for flight control design
Dynamic blade shape for improved helicopter rotor performance
Nutzung des A340-Simulators für Flugeigenschaftsanalysen
Control mechanism strategies for spin-stabilized projectiles
First steps in the development of handling qualities criteria for a civil tilt rotor