ANALYSIS OF ROCKET-ENGINE TRANSIENT REGIMES

被引:3
作者
BARRERE, M [1 ]
机构
[1] OFF NATL ETUD & RECH AEROSP,F-92320 CHATILLON,FRANCE
关键词
D O I
10.1016/0094-5765(77)90113-8
中图分类号
V [航空、航天];
学科分类号
08 ; 0825 ;
摘要
引用
收藏
页码:641 / 670
页数:30
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共 18 条
[11]   CALCULATION OF ACOUSTIC ADMITTANCE AT A BURNING SURFACE [J].
RYAZANTSEV, YS ;
TULSKIH, VE .
ACTA ASTRONAUTICA, 1976, 3 (3-4) :171-185
[12]  
Sirignano, 1969, COMBUST SCI TECHNOL, V1, DOI [10.1080/00102206908952190, DOI 10.1080/00102206908952190]
[14]   THEORY OF DYNAMIC EXTINGUISHMENT OF SOLID PROPELLANTS WITH SPECIAL REFERENCE TO NONSTEADY HEAT FEEDBACK LAW [J].
SUMMERFIELD, M ;
CAVENY, LH ;
BATTISTA, RA ;
KUBOTA, N ;
GOSTINTS.YA ;
ISODA, H .
JOURNAL OF SPACECRAFT AND ROCKETS, 1971, 8 (03) :251-+
[16]  
WILLIAMS FA, 1969, AGARD116
[17]  
ZINN BT, 1968, ASTRONAUT ACTA, V13, P489
[18]  
1976, JOURNEE ETUDE PROPUL