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OPTIMAL DESIGN AND AERODYNAMIC CALCULATION OF WING CONFIGURATION OF CIVIL AIRCRAFT

南京航空航天大学学报:英文版Issue(2):P.165-169,5.
南京航空航天大学学报:英文版Issue(2):P.165-169,5.

OPTIMAL DESIGN AND AERODYNAMIC CALCULATION OF WING CONFIGURATION OF CIVIL AIRCRAFT

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optimum design aerodynamic computations civil aircraft sheared wing-tip wing penalty function

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航空航天

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..OPTIMAL DESIGN AND AERODYNAMIC CALCULATION OF WING CONFIGURATION OF CIVIL AIRCRAFT[J].南京航空航天大学学报:英文版,1994,(2):P.165-169,5.

南京航空航天大学学报:英文版

1005-1120

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