DEVELOPMENT OF A LINEAR UNSTEADY AERODYNAMIC ANALYSIS FOR FINITE-DEFLECTION SUBSONIC CASCADES

被引：28
作者：
VERDON, JM
CASPAR, JR
机构：
来源：
AIAA JOURNAL | 1982年 / 20卷 / 09期
关键词：
D O I：
10.2514/3.51186
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：1259 / 1267
页数：9
相关论文
共 14 条
[1]  
Abbott H., 1959, DOVER BOOKS AERONAUT
[2]  
ASHLEY H, 1965, AERODYNAMICS WINGS B, P93
[3]  
ATASSI H, 1978, AIAA78227 PAP
[4]  
CARUTHERS JE, 1981, AEROELASTICITY TURBO, P31
[5]   CALCULATION OF TWO-DIMENSIONAL POTENTIAL CASCADE FLOW USING FINITE AREA METHODS [J].
CASPAR, JR ;
HOBBS, DE ;
DAVIS, RL .
AIAA JOURNAL, 1980, 18 (01) :103-109
[6]   NUMERICAL TREATMENT OF UNSTEADY SUBSONIC FLOW PAST AN OSCILLATING CASCADE [J].
CASPAR, JR ;
VERDON, JM .
AIAA JOURNAL, 1981, 19 (12) :1531-1539
[7]  
FUNG YC, 1955, INTRO THEORY AEROELA, P166
[8]   UNSTEADY VORTICAL AND ENTROPIC DISTORTIONS OF POTENTIAL FLOWS ROUND ARBITRARY OBSTACLES [J].
GOLDSTEIN, ME .
JOURNAL OF FLUID MECHANICS, 1978, 89 (DEC) :433-468
[9]   2ND-ORDER ACCURATE CALCULATION OF TRANSONIC FLOW OVER TURBOMACHINERY CASCADES [J].
IVES, DC ;
LIUTERMOZA, JF .
AIAA JOURNAL, 1979, 17 (08) :870-876
[10]  
Mikolajczak A., 1975, AIAA J AIRCRAFT, V12, P325, DOI [10.2514/3.44451, DOI 10.2514/3.44451]
12