WING CONFIGURATION EFFECTS ON FLOW FIELD AND AERODYNAMIC PER-FORMANCE OF SUPERSONIC BIPLANE FOR SONIC-BOOM REDUCTION
International congress; 26th, International Council of the Aeronautical Sciences; 8th AIAA Aviation Technology, Integration, and Operations (ATIO) ; 2008 ; Anchorage, Alaska
01.01.2008
9 pages
Held on CD-ROM. Also Known as ICAS 2008; Held in e-store (RMS)
Aufsatz (Konferenz)
Englisch
© Metadata Copyright the British Library Board and other contributors. All rights reserved.
Design of Supersonic Biplane Aircraft Concerning Sonic Boom Minimization
British Library Conference Proceedings | 2010
|British Library Conference Proceedings | 2011
|