A NEW EFFICIENT CONTROL METHOD FOR BLENDED WING BODY
نویسندگان
چکیده
منابع مشابه
TITLE AND SUBTITLE A Method for Designing Blended Wing - Body Con gurations for
A procedure for tailoring a blended wing-body con guration to reduce its computed wave drag is described. The method utilizes an iterative algorithm within the framework of rst-order linear theory. Four computed examples are included. In each case, the zero-lift wave drag was reduced without an increase in drag due to lift. Introduction In the initial rough-cut state of supersonic conguration d...
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ژورنال
عنوان ژورنال: International Journal of Modern Physics: Conference Series
سال: 2012
ISSN: 2010-1945,2010-1945
DOI: 10.1142/s2010194512008999