Influence of small angles of attack and sweep on the rolling moment at a hypersonic flow around the bodies of revolution

被引：0

作者：

Mokin, Yu. A. ^{[1
]}

机构：

[1] State Rocket Ctr Makeyev, Construct Bur, Miass, Russia

来源：

THERMOPHYSICS AND AEROMECHANICS | 2009年 / 16卷 / 01期

关键词：

hypersonic flow; body of revolution; small variations of surface; angle of attack; rolling moment;

D O I：

暂无

中图分类号：

V [航空、航天];

学科分类号：

08 ; 0825 ;

摘要：

The influence of small attack and sweep angles on the rolling moment variation at a supersonic flow around the bodies close to the bodies of revolution is considered. Based on the method of the differential hypothesis of locality the integral expressions are obtained for the derivatives of the rolling moment coefficient with respect to the attack and sweep angles. The norm of these derivatives is defined and the estimates for the norm are obtained.

引用

页码：37 / 42

页数：6

共 50 条

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Mokin Yu.A.
[J]. Thermophysics and Aeromechanics, 2009, 16 (1) : 37 - 42
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[8] GAS FLOW PAST NONAXISYMMETRIC BODIES AT SMALL ANGLES OF ATTACK
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[9] LIMITING HYPERSONIC FLOW NEAR THE STAGNATION POINT OF BODIES OF REVOLUTION AT ANGLE OF ATTACK
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[J]. CONTINUUM MECHANICS AND ITS APPLICATIONS, 1989, : 667 - 678
[10] AN APPROXIMATE TREATMENT OF MULTISHOCK BODIES OF REVOLUTION AT SMALL ANGLES OF ATTACK BY THE METHOD OF CHARACTERISTICS
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