CARTESIAN MESH SOLUTION FOR AXISYMMETRIC TRANSONIC POTENTIAL FLOW AROUND INLETS

被引:9
作者
REYHNER, TA [1 ]
机构
[1] BOEING COMMERCIAL AIRPLANE CO,SEATTLE,WA
关键词
D O I
10.2514/3.60670
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:624 / 631
页数:8
相关论文
共 17 条
[1]   CALCULATION OF TRANSONIC FLOW AROUND AXISYMMETRIC INLETS [J].
ARLINGER, BG .
AIAA JOURNAL, 1975, 13 (12) :1614-1621
[2]  
BAILEY FR, 1975, SP347 NASA 2, P1213
[3]  
BOPPE CW, 1977, AIAA77207 PAP
[4]  
CARLSON L.A., 1976, J AIRCRAFT, V13, P349
[5]  
CAUGHEY DA, 1976, AIAA76100 PAP
[6]  
COLEHOUR JJ, 1973, AIAA73657 PAP
[7]   CONVERGENCE ACCELERATION OF RELAXATION SOLUTIONS FOR TRANSONIC FLOW COMPUTATIONS [J].
HAFEZ, MM ;
CHENG, HK .
AIAA JOURNAL, 1977, 15 (03) :329-336
[8]  
HAFEZ MM, 1975, AIAA7551 PAP
[9]   ITERATIVE SOLUTION OF TRANSONIC FLOWS OVER AIRFOILS AND WINGS, INCLUDING FLOWS AT MACH 1 [J].
JAMESON, A .
COMMUNICATIONS ON PURE AND APPLIED MATHEMATICS, 1974, 27 (03) :283-309
[10]  
Jameson A, 1973, P AIAA COMPUTATIONAL, P18