AERODYNAMIC CHARACTERISTICS OF THE THIN DELTA WING FITTED WITH A CONICAL BODY IN SUPERSONIC FLOW.

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作者
Nastase, Adriana
Paraschivoiu, Ion
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中图分类号
V211 [空气动力学]; V411 [空气动力学];
学科分类号
0801 ; 080103 ; 080104 ;
摘要
The paper deals with the determination of the influence of the presence of a central conical body without incidence on the aerodynamic characteristics of a thin delta wing with supersonic leading edges. The downwash on the wing is considered expressed under the form of a homogeneous polynomial of second order.
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页码:963 / 989
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