A Low Fidelity Method for Flap Aerodynamic Design of a Cranked-Arrow Wing
25th AIAA Applied Aerodynamics Conference
2007-01-01
Conference paper
Electronic Resource
English
A Low Fidelity Method for Flap Aerodynamic Design of a Cranked-Arrow Wing
British Library Conference Proceedings | 2007
|Dynamic Ground Effect for a Cranked Arrow Wing Airplane
NTIS | 1997
|