DIFFRACTION OF A WEAK SHOCK WITH VORTEX GENERATION

被引:126
作者
ROTT, N
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D O I
10.1017/S0022112056000081
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O3 [力学];
学科分类号
08 ; 0801 ;
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页码:111 / 128
页数:18
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共 12 条
[1]   EFFECT OF LEADING-EDGE SEPARATION ON THE LIFT OF A DELTA-WING [J].
BROWN, CE ;
MICHAEL, WH .
JOURNAL OF THE AERONAUTICAL SCIENCES, 1954, 21 (10) :690-&
[2]   AERODYNAMICS OF A RECTANGULAR PLATE WITH VORTEX SEPARATION IN SUPERSONIC FLOW [J].
CHENG, HK .
JOURNAL OF THE AERONAUTICAL SCIENCES, 1955, 22 (04) :217-226
[3]  
EDWARDS RH, 1954, J AERONAUT SCI, V21, P134
[4]   THE DIFFRACTION OF SOUND PULSES .1. DIFFRACTION BY A SEMI-INFINITE PLANE [J].
FRIEDLANDER, FG .
PROCEEDINGS OF THE ROYAL SOCIETY OF LONDON SERIES A-MATHEMATICAL AND PHYSICAL SCIENCES, 1946, 186 (1006) :322-344
[5]  
HOARD LN, 1955, 11 PRINC U TECHN REP
[6]  
Kaden H., 1931, ING ARCH, V2, P140, DOI 10.1007/BF02079924
[7]   DIFFRACTION AND REFLECTION OF PULSES BY WEDGES AND CORNERS [J].
KELLER, JB ;
BLANK, A .
COMMUNICATIONS ON PURE AND APPLIED MATHEMATICS, 1951, 4 (01) :75-94
[8]  
MICHAEL WH, 1955, 3472 NAT ADV COMM AE
[9]   ON THE DIFFRACTION OF AN ACOUSTIC PULSE BY A WEDGE [J].
MILES, JW .
PROCEEDINGS OF THE ROYAL SOCIETY OF LONDON SERIES A-MATHEMATICAL AND PHYSICAL SCIENCES, 1952, 212 (1111) :543-547
[10]  
Prandtl L, 1922, VORTRAGE GEBIETE HYD