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BOUNDARY-LAYER FLOWS WITH LARGE INJECTION AND HEAT TRANSFER

被引：38
作者：
KUBOTA, T
FERNANDEZ, FL
机构：
来源：
AIAA JOURNAL | 1968年 / 6卷 / 01期
关键词：
D O I：
10.2514/3.4436
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：22 / +
页数：1
相关论文
共 9 条
[1]  
AROESTY J, 1965, RM4620ARPA RAND CORP
[2]  
COHEN CB, 1956, TN1295 NACA
[3]   SUPERSONIC SEPARATED AND REATTACHING LAMINAR FLOWS .1. GENERAL THEORY AND APPLICATION TO ADIABATIC BOUNDARY-LAYER-SHOCK-WAVE INTERACTIONS [J].
LEES, L ;
REEVES, BL .
AIAA JOURNAL, 1964, 2 (11) :1907-1920
[4]   LAMINAR HEAT TRANSFER OVER BLUNT-NOSED BODIES AT HYPERSONIC FLIGHT SPEEDS [J].
LEES, L .
JET PROPULSION, 1956, 26 (04) :259-&
[5]   THE HOMOGENEOUS BOUNDARY LAYER AT AN AXISYMMETRIC STAGNATION POINT WITH LARGE RATES OF INJECTION [J].
LIBBY, PA .
JOURNAL OF THE AEROSPACE SCIENCES, 1962, 29 (01) :48-60
[6]   REMARKS ON QUASILINEARIZATION APPLIED IN BOUNDARY-LAYER CALCULATIONS [J].
LIBBY, PA ;
CHEN, KK .
AIAA JOURNAL, 1966, 4 (05) :937-&
[7]   Limits of limnial layers influnce [J].
Pretsch, J .
ZEITSCHRIFT FUR ANGEWANDTE MATHEMATIK UND MECHANIK, 1944, 24 :264-267
[8]   APPLICATION OF QUASILINEARIZATION TO BOUNDARY-LAYER EQUATIONS [J].
RADBILL, JR .
AIAA JOURNAL, 1964, 2 (10) :1860-1862
[9]  
WHITTAKER ET, 1963, MODERN ANALYSIS
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