EXPERIMENTS ON BOUNDARY-LAYER TRANSITION AT SUPERSONIC SPEEDS

被引:30
作者
VANDRIEST, ER
BOISON, JC
机构
来源
JOURNAL OF THE AERONAUTICAL SCIENCES | 1957年 / 24卷 / 12期
关键词
D O I
10.2514/8.3994
中图分类号
V [航空、航天];
学科分类号
08 ; 0825 ;
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页码:885 / 899
页数:15
相关论文
共 6 条
[1]   LENS SYSTEM PRODUCING UNEQUAL MAGNIFICATION IN 2 MUTUALLY PERPENDICULAR DIRECTIONS [J].
BUCHELE, DR ;
GOOSSENS, HR .
REVIEW OF SCIENTIFIC INSTRUMENTS, 1954, 25 (03) :262-263
[2]   REVIEW OF PUBLISHED DATA ON THE EFFECT OF ROUGHNESS ON TRANSITION FROM LAMINAR TO TURBULENT FLOW [J].
DRYDEN, HL .
JOURNAL OF THE AERONAUTICAL SCIENCES, 1953, 20 (07) :477-482
[3]  
LEES L, 1947, NACA TR876
[4]  
PUCKETT AE, 1953, SWT12T5 CALTECH JET
[5]   CALCULATION OF THE STABILITY OF THE LAMINAR BOUNDARY LAYER IN A COMPRESSIBLE FLUID ON A FLAT PLATE WITH HEAT TRANSFER [J].
VANDRIEST, ER .
JOURNAL OF THE AERONAUTICAL SCIENCES, 1952, 19 (12) :801-&
[6]  
VANDRIEST ER, 1952, NACA TN2597