AN APPROXIMATE SOLUTION OF THE DIRECT SUPERSONIC BLUNT-BODY PROBLEM FOR ARBITRARY AXISYMMETRIC SHAPES

被引:21
作者
TRAUGOTT, SC
机构
来源
JOURNAL OF THE AEROSPACE SCIENCES | 1960年 / 27卷 / 05期
关键词
D O I
10.2514/8.8540
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:361 / 370
页数:10
相关论文
共 23 条
[1]  
BELOTSERKOVSKY OM, 1957, DOKL AKAD NAUK SSSR+, V113, P509
[2]   AN EXPERIMENTAL INVESTIGATION OF BLUNT BODY STAGNATION POINT VELOCITY GRADIENT [J].
BOISON, JC ;
CURTISS, HA .
ARS JOURNAL, 1959, 29 (02) :130-135
[3]  
BUSEMANN A, 1949, NACA TN1858
[4]  
CABANNES H, 1951, ONERA TN5
[6]   ON THE NUMERICAL CALCULATION OF DETACHED BOW SHOCK WAVES IN HYPERSONIC FLOW [J].
GARABEDIAN, PR ;
LIEBERSTEIN, HM .
JOURNAL OF THE AERONAUTICAL SCIENCES, 1958, 25 (02) :109-118
[7]  
HASTINGS SM, 1957, NAVORD5659 REP
[8]  
HAYES WD, 1955, SOME ASPECTS HYPERSO
[9]  
HEBERLE JW, 1950, NACA TN2000
[10]   INVESTIGATION OF LOCAL LAMINAR HEAT TRANSFER ON A HEMISPHERE FOR SUPERSONIC MACH NUMBERS AT LOW RATES OF HEAT FLUX [J].
KOROBKIN, I ;
GRUENEWALD, KH .
JOURNAL OF THE AERONAUTICAL SCIENCES, 1957, 24 (03) :188-194