UNSTEADY AERODYNAMICS OF A FINITE SUPERSONIC CASCADE WITH SUBSONIC AXIAL-FLOW

被引:12
作者
VERDON, JM [1 ]
机构
[1] UNITED AIRCRAFT RES LABS,E HARTFORD,CT 06108
来源
JOURNAL OF APPLIED MECHANICS-TRANSACTIONS OF THE ASME | 1973年 / 40卷 / 03期
关键词
Compendex;
D O I
10.1115/1.3423070
中图分类号
O3 [力学];
学科分类号
08 ; 0801 ;
摘要
Degrees of freedom (mechanics)
引用
收藏
页码:667 / 671
页数:5
相关论文
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[1]  
Ashley H., 1965, AERODYNAMICS WINGS B
[2]  
Fung Y.C, 2002, INTRO THEORY AEROELA
[3]  
LANE F, 1957, J AERONAUT SCI, V24, P65
[4]  
Miles John W., 1959, POTENTIAL THEORY UNS
[5]   THE COMPRESSIBLE FLOW PAST AN OSCILLATING AIRFOIL IN A WIND TUNNEL [J].
MILES, JW .
JOURNAL OF THE AERONAUTICAL SCIENCES, 1956, 23 (07) :671-678