COMPUTATIONAL INVESTIGATION OF OBLIQUE DETONATION RAMJET-IN-TUBE CONCEPTS

被引:22
作者
BRACKETT, DC
BOGDANOFF, DW
机构
关键词
D O I
10.2514/3.23149
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:276 / 281
页数:6
相关论文
共 10 条
[1]  
BOGDANOFF DW, IN PRESS AIAA J
[2]  
BOGDANOFF DW, 1987, AIAA871978 PAP
[3]  
BRUCKNER AP, 1987, AIAA871327 PAP
[4]   RAM ACCELERATOR - A NEW CHEMICAL METHOD FOR ACCELERATING PROJECTILES TO ULTRAHIGH VELOCITIES [J].
HERTZBERG, A ;
BRUCKNER, AP ;
BOGDANOFF, DW .
AIAA JOURNAL, 1988, 26 (02) :195-203
[5]  
HERTZBERG A, 1988, 16 INT S SHOCK WAV, P117
[6]  
Jeromin L., 1970, PROG AEROSP SCI, V10, P65, DOI [10.1016/0376-0421(70)90004-7, DOI 10.1016/0376-0421(70)90004-7]
[7]  
KNOWLEN C, 1987, AIAA872152 PAP
[8]  
KNUTH EL, 1963, INT J HEAT MASS TRAN, V6, P999
[9]  
STULL DR, 1971, NSRDSNBS37, P4
[10]   TURBULENT BOUNDARY LAYER IN COMPRESSIBLE FLUIDS [J].
VANDRIEST, ER .
JOURNAL OF THE AERONAUTICAL SCIENCES, 1951, 18 (03) :145-&