Unsteady pressure behavior in a Ramjet/Scramjet inlet

被引：74
作者：
Rodi, PE
Emami, S
Trexler, CA
机构：
[1] LOCKHEED ENGN & SCI CO,NASA,LANGLEY RES CTR,HAMPTON,VA 23681
[2] NASA,LANGLEY RES CTR,GAS DYNAM DIV,HAMPTON,VA 23681
来源：
JOURNAL OF PROPULSION AND POWER | 1996年 / 12卷 / 03期
关键词：
D O I：
10.2514/3.24061
中图分类号：
V [航空、航天];
学科分类号：
08 ; 0825 ;
摘要：
Mean and time-accurate pressures have been measured in the inlet of a dual-mode, ramjet/scramjet configuration. This configuration was designed for low hypersonic Mach number operation using a hydrocarbon based fuel. The time accurate measurements are presented for inlets operating at maximum permissible back-pressure during and after inlet unstart.
引用
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页码：486 / 493
页数：8
相关论文
共 16 条
[1]  
ANDREWS EH, 1994, 942817 AIAA
[2]  
Bendat J., 2010, Random data: analysis and measurement procedures
[3]  
BILLIG FS, 1990, CP AGARD, V479
[4]  
BILLIG FS, 1991, HIGH SPEED FLIGHT PR, P21
[5]  
Curran E. T., 1964, RTDTDR634097 AER PRO
[6]  
Dolling D. S., 1993, AIAA Paper 93-0284
[7]  
Emami S., 1995, TP3502 NASA
[8]  
HARDIN JC, 1986, RP1145 NASA
[9]  
KEY I, 1991, J PROPULSION POWER, V8, P507
[10]   COMPARISON OF SHOCK-INDUCED 2-DIMENSIONAL AND 3-DIMENSIONAL INCIPIENT TURBULENT SEPARATION [J].
KORKEGI, RH .
AIAA JOURNAL, 1975, 13 (04) :534-535
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