EXPERIMENTAL-DETERMINATION OF DISCHARGE COEFFICIENTS FOR CRITICAL FLOW THROUGH AN AXISYMMETRIC NOZZLE

被引:39
作者
TANG, SP [1 ]
机构
[1] YALE UNIV,DEPT ENGN & APPL SCI,NEW HAVEN,CT 06520
关键词
D O I
10.2514/3.60854
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:41 / 46
页数:6
相关论文
共 26 条
[1]  
ARNBERG BT, 1961, J BASIC ENGINEERING, V84, P447
[2]   TRANSONIC LAMINAR BOUNDARY-LAYERS WITH SURFACE CURVATURE [J].
BACK, LH .
INTERNATIONAL JOURNAL OF HEAT AND MASS TRANSFER, 1973, 16 (09) :1745-1761
[3]   COMPRESSIBLE LAMINAR BOUNDARY-LAYERS WITH LARGE ACCELERATION AND COOLING [J].
BACK, LH ;
CUFFEL, RF .
AIAA JOURNAL, 1976, 14 (07) :968-971
[4]   INFLUENCE OF CONTRACTION SECTION SHAPE AND INLET FLOW DIRECTION ON SUPERSONIC NOZZLE FLOW AND PERFORMANCE [J].
BACK, LH ;
MASSIER, PF ;
CUFFEL, RF .
JOURNAL OF SPACECRAFT AND ROCKETS, 1972, 9 (06) :420-+
[5]   PREDICTION OF HEAT TRANSFER FROM LAMINAR BOUNDARY LAYERS WITH EMPHASIS ON LARGE FREE-STREAM VELOCITY GRADIENTS AND HIGHLY COOLED WALLS [J].
BACK, LH ;
WITTE, AB .
JOURNAL OF HEAT TRANSFER, 1966, 88 (03) :249-&
[7]   FLOW COEFFICIENTS FOR SUPERSONIC NOZZLES WITH COMPARATIVELY SMALL RADIUS OF CURVATURE THROATS [J].
BACK, LH ;
CUFFEL, RF .
JOURNAL OF SPACECRAFT AND ROCKETS, 1971, 8 (02) :196-&
[8]   COMPARISON OF MEASURED AND PREDICTED FLOWS THROUGH CONICAL SUPERSONIC NOZZLES WITH EMPHASIS ON TRANSONIC REGION [J].
BACK, LH ;
MASSIER, PF ;
GIER, HL .
AIAA JOURNAL, 1965, 3 (09) :1606-&
[9]  
BACK LH, 1970, AIAA J, V8, P2066
[10]   COMPUTATION OF 2-DIMENSIONAL, VISCOUS NOZZLE-FLOW [J].
CLINE, MC .
AIAA JOURNAL, 1976, 14 (03) :295-296