AEROTHERMOCHEMICAL ANALYSIS OF EROSIVE BURNING IN A LABORATORY SOLID-ROCKET MOTOR

被引：18
作者：
BEDDINI, RA
机构：
来源：
AIAA JOURNAL | 1980年 / 18卷 / 11期
关键词：
D O I：
10.2514/3.50890
中图分类号：
V [航空、航天];
学科分类号：
08 ; 0825 ;
摘要：
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页码：1346 / 1353
页数：8
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共 21 条
[1]   REACTING TURBULENT BOUNDARY-LAYER APPROACH TO SOLID-PROPELLANT EROSIVE BURNING [J].
BEDDINI, RA .
AIAA JOURNAL, 1978, 16 (09) :898-905
[2]  
BEDDINI RA, 1977, ARAP7711 AER RES ASS
[3]  
BORGHI R, 1979, 17TH S INT COMB, P235
[4]  
BORGHI R, 1974, ADV GEOPHYS B, V18, P349
[5]  
CAVENY LH, 1978, COMMUNICATION 0619
[6]   ROTATIONAL AXISYMMETRIC MEAN FLOW AND DAMPING OF ACOUSTIC WAVES IN A SOLID PROPELLANT ROCKET [J].
CULICK, FEC .
AIAA JOURNAL, 1966, 4 (08) :1462-&
[7]   FLOWFIELD IN COMBUSTION CHAMBER OF A SOLID-PROPELLANT ROCKET MOTOR [J].
DUNLAP, R ;
WILLOUGH.PG ;
HERMSEN, RW .
AIAA JOURNAL, 1974, 12 (10) :1440-1442
[8]  
HINZE JO, 1975, TURBULENCE, P614
[9]  
HUESMANN K, 1968, WARME STOFFUBERTRAGU, V1, pS2
[10]   MODEL OF EROSIVE BURNING OF COMPOSITE PROPELLANTS [J].
KING, MK .
JOURNAL OF SPACECRAFT AND ROCKETS, 1978, 15 (03) :139-146
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