RADIATIVE IGNITION OF DOUBLE BASE PROPELLANTS .2. PRE-IGNITION EVENTS AND SOURCE EFFECTS

被引:33
作者
DELUCA, L [1 ]
OHLEMILLER, TJ [1 ]
CAVENY, LH [1 ]
SUMMERFIELD, M [1 ]
机构
[1] PURDUE UNIV,W LAFAYETTE,IN 47907
关键词
D O I
10.2514/3.7193
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:1111 / 1117
页数:7
相关论文
共 18 条
[11]   SITE AND MODE OF ACTION OF PLATONIZERS IN DOUBLE BASE PROPELLANTS [J].
KUBOTA, N ;
OHLEMILL.TJ ;
CAVENY, LH ;
SUMMERFI.M .
AIAA JOURNAL, 1974, 12 (12) :1709-1714
[12]  
LIBROVICH VB, 1963, ZH PRIKLADNOI MEKHAN, V6, P74
[13]   PROPELLANT COMBUSTION INSTABILITY AS MEASURED BY COMBUSTION RECOIL [J].
MIHLFEITH, CM ;
RYAN, NW ;
BAER, AD .
AIAA JOURNAL, 1972, 10 (10) :1280-+
[14]  
MIHLFIETH CM, 1971, TR712664 U UT AIR FO
[15]  
OHLEMILLER TJ, 1973, 14TH S INT COMB PITT, P1297
[16]  
PRICE EW, 1964, AIAA65120 PAP
[17]  
SHANNON LJ, 1967, AFOSR671765 AIR FORC
[18]  
ZELDOVICH YB, 1963, DOKLADY ADADEMIIA NU, V2, P150