A UNIFORMLY VALID ASYMPTOTIC SOLUTION FOR UNSTEADY SUBRESONANT FLOW THROUGH SUPERSONIC CASCADES

被引：2
作者：
BENDIKSEN, OO
机构：
来源：
AIAA JOURNAL | 1984年 / 22卷 / 01期
关键词：
D O I：
10.2514/3.8360
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：154 / 157
页数：4
相关论文
共 7 条
[1]   COUPLED BENDING-TORSION FLUTTER IN A SUPERSONIC CASCADE [J].
BENDIKSEN, O ;
FRIEDMANN, P .
AIAA JOURNAL, 1981, 19 (06) :774-781
[2]  
BENDIKSEN O, 1980, THESIS U CALIFORNIA
[3]  
BENDIKSEN OO, 1980, UCLA ENG8072 REPT
[4]   UNSTEADY SUPERSONIC CASCADE WITH A SUBSONIC LEADING-EDGE - EXACT FIRST-ORDER THEORY .1. [J].
KUROSAKA, M .
JOURNAL OF ENGINEERING FOR POWER-TRANSACTIONS OF THE ASME, 1974, 96 (01) :13-22
[5]  
NAGASHIMA T, 1978, RM3811 GREAT BRIT AE
[6]  
STRADA JA, 1978, ASME78GT151 PAP
[7]   FURTHER DEVELOPMENTS IN AERODYNAMIC ANALYSIS OF UNSTEADY SUPERSONIC CASCADES .1. UNSTEADY PRESSURE FIELD [J].
VERDON, JM .
JOURNAL OF ENGINEERING FOR POWER-TRANSACTIONS OF THE ASME, 1977, 99 (04) :509-516
1