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
2008-01-01
9 pages
Held on CD-ROM. Also Known as ICAS 2008; Held in e-store (RMS)
Conference paper
English
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Design of Supersonic Biplane Aircraft Concerning Sonic Boom Minimization
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