The thermal correction of the inlet diffuser of a hypersonic scramjet engine

被引：0
|
作者：
Bormotova, TA [1 ]
Volodin, VV
Golub, VV
Laskin, IN
机构：
[1] Russian Acad Sci, Inst High Energy Dens, IVTAN Inst High Temp Sci Assoc, Moscow 125412, Russia
[2] Cent Inst Aviat Motors, Moscow 111250, Russia
来源：
HIGH TEMPERATURE | 2003年 / 41卷 / 03期
关键词：
Statistical Physic; Thermal Correction; Scramjet Engine; Inlet Diffuse; Hypersonic Scramjet;
D O I：
10.1023/A:1024259130915
中图分类号：
O59 [应用物理学];
学科分类号：
摘要：
引用
收藏
页码：415 / 416
页数：2
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