AIAA 2006-1205 A Coupled Approach for Plasma-Based Flow Control Simulations of Wing Sections
44th, Aerospace sciences meeting ; 2006 ; Reno, NV
Aerospace sciences meeting ; 14658-14677
2006-01-01
20 pages
VOL 19 of 24 VOLS
Aufsatz (Konferenz)
Englisch
© Metadata Copyright the British Library Board and other contributors. All rights reserved.
AIAA-2001-1205 Composite Wing Structural Design Optimization with Continuity Constraints
British Library Conference Proceedings | 2001
|British Library Conference Proceedings | 2014
|AIAA 2006-0877 Simulations of Flow Separation Control Using Plasma Actuators
British Library Conference Proceedings | 2006
|