similitude of hypersonic flow
高超声速相似律
THE AERODYNAMICAL ANALYSIS OF BODY IN HYPERSONIC SOURCE FLOW FIELD
高超声速点泉流场中的气动力
Numerical study of flow past hypersonic research vehicle with detaching booster
高超声速验证飞行器助推分离段流场数值研究
Flutter of Airfoil with Structural Nonlinearity in Supersonic and Hypersonic Flow
结构非线性机翼的超音速和高超音速颤振
The computation and analysis for the hypersonic flow over reentry vehicles with ablation
高超声速再入体烧蚀流场计算分析
Firstly, the steady laminar flow field of a hypersonic sharp cone boundary layer with zero angle of attack was computed.
先计算出高超音速零攻角尖锥边界层的定常层流流场。
Stability Characteristics of the Boundary Layer of an Axisymmetric Blunt Nosed Cone in the Supersonic and Hypersonic Flow
超声速高超声速球锥绕流的边界层稳定性特点初探
This paper presents the separation shock motion features induced by a hemicylindrically blunted fin in a hypersonic turbulent flow.
给出半圆柱前缘舵诱导的高超声速湍流分离激波运动特性。
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