ESTIMATION OF HEAT-TRANSFER COEFFICIENT IN A ROCKET NOZZLE

被引:7
作者
MEHTA, RC
机构
关键词
D O I
10.2514/3.7846
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:1085 / 1086
页数:2
相关论文
共 12 条
[1]  
BARTZ DR, 1957, JET PROPULSION, V27, P49
[2]   SURFACE HEAT FLUX DETERMINATION USING AN INTEGRAL METHOD [J].
BECK, JV .
NUCLEAR ENGINEERING AND DESIGN, 1968, 7 (02) :170-&
[4]  
BRINSMADE AF, 1965, HEAT TRANSFER CHEM E, V61, P88
[5]  
BURGGRAF OR, 1964, J HEAT TRANSFER, V86, P378
[6]   PREDICTION OF TRANSIENT TEMPERATURE DISTRIBUTIONS WITH EMBEDDED THERMOCOUPLES [J].
IMBER, M ;
KHAN, J .
AIAA JOURNAL, 1972, 10 (06) :784-+
[7]  
MEHTA RC, 1977, AIAA J, V9, P1355
[8]  
Powell W., 1964, ISA T, V3, P246
[9]  
Sparrow E. M., 1964, J APPLIED MECHANICS, V86, P369
[10]  
Stolz G., 1960, J HEAT TRANSF, V82, P20, DOI [10.1115/1.3679871, DOI 10.1115/1.3679871]