再人飞行器脉动压力环境的分析与预测

IMECH-IR > 力学所知识产出(1956-2008)

	再人飞行器脉动压力环境的分析与预测
	徐立功; 刘振寰
Source Publication	空气动力学学报
	1991
Volume	9 Issue:4 Pages:457-464
ISSN	0258-1825
Abstract	本文分析了机动再入飞行器因非定常空气动力流动引起的物面脉动压力环境,并根据高超声速无粘流计算的表面压力分布,给出了一套预测各种脉动压力环境统计特性的工程计算公式。算例表明,预测的均方根脉动压力、功率谱密度和交叉功率谱密度与实验值是一致的。
Keyword	机动再入飞行器脉动压力功率谱密度交叉功率谱密度激波振荡
Language	中文
Document Type	期刊论文
Identifier	http://dspace.imech.ac.cn/handle/311007/36122
Collection	力学所知识产出(1956-2008)
Corresponding Author	徐立功
Recommended Citation GB/T 7714	徐立功,刘振寰. 再人飞行器脉动压力环境的分析与预测[J]. 空气动力学学报,1991,9,4,:457-464.
APA	徐立功,&刘振寰.(1991).再人飞行器脉动压力环境的分析与预测.空气动力学学报,9(4),457-464.
MLA	徐立功,et al."再人飞行器脉动压力环境的分析与预测".空气动力学学报 9.4(1991):457-464.

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