NUMERICAL-SOLUTION OF SUPERSONIC PANEL FLUTTER EIGENPROBLEM

被引:6
作者
GUPTA, KK [1 ]
机构
[1] CALTECH JET PROP LAB,PASADENA,CA 91103
关键词
D O I
10.1002/nme.1620100312
中图分类号
T [工业技术];
学科分类号
08 ;
摘要
引用
收藏
页码:637 / 645
页数:9
相关论文
共 11 条
[1]  
ARGYRIS JH, 1972, ASTRONAUTICAL RES, P179
[2]  
Fox L., 1965, An Introduction to Numerical Linear Algebra
[3]  
Gupta K. K., 1972, International Journal for Numerical Methods in Engineering, V4, P379, DOI 10.1002/nme.1620040308
[4]  
Gupta K. K., 1973, International Journal for Numerical Methods in Engineering, V7, P17, DOI 10.1002/nme.1620070103
[5]  
Gupta K. K., 1970, International Journal for Numerical Methods in Engineering, V2, P221, DOI 10.1002/nme.1620020207
[6]  
GUPTA KK, 1969, INT J NUM METH ENGNG, V5, P351
[7]   FINITE ELEMENTS APPLIED TO PANEL FLUTTER [J].
OLSON, MD .
AIAA JOURNAL, 1967, 5 (12) :2267-&
[8]   SOME FLUTTER SOLUTIONS USING FINITE ELEMENTS [J].
OLSON, MD .
AIAA JOURNAL, 1970, 8 (04) :747-+
[9]  
Sander G., 1973, International Journal for Numerical Methods in Engineering, V7, P379, DOI 10.1002/nme.1620070313
[10]  
Wilkinson J.H., 1988, The Algebraic Eigenvalue Problem