Rolling Moment Characteristics at High Alpha on Several Planforms of Cranked Arrow Wing Configuration
27th, AIAA Applied Aerodynamics Conference ; 2009 ; San Antonio, TX
2009-01-01
9 pages
Conference paper
English
© Metadata Copyright the British Library Board and other contributors. All rights reserved.
Computational Transonic Flutter Solutions for Cranked Wing Planforms (AIAA 2014-0674)
British Library Conference Proceedings | 2014
|Dynamic Ground Effect for a Cranked Arrow Wing Airplane
NTIS | 1997
|