VIBRATION MEASUREMENTS OF AN AIRPLANE FUSELAGE STRUCTURE .2. JET NOISE EXCITATION

被引:24
作者
WILBY, JF
GLOYNA, FL
机构
关键词
D O I
10.1016/0022-460X(72)90504-4
中图分类号
O42 [声学];
学科分类号
070206 ; 082403 ;
摘要
引用
收藏
页码:467 / &
相关论文
共 10 条
[3]  
BULL MK, 1963, AASU243 U SOUTH REP
[4]  
Clarkson B. L., 1962, J ROYAL AERONAUTICAL, V66, P603, DOI [10.1017/S000192400008934X, DOI 10.1017/S000192400008934X]
[5]   A BRIEF SURVEY OF TRANSFER MATRIX TECHNIQUES WITH SPECIAL REFERENCE TO ANALYSIS OF AIRCRAFT PANELS [J].
LIN, YK ;
DONALDSON, BK .
JOURNAL OF SOUND AND VIBRATION, 1969, 10 (01) :103-+
[6]   STRESSES IN CONTINUOUS SKIN-STIFFENER PANELS UNDER RANDOM LOADING [J].
LIN, YK .
JOURNAL OF THE AEROSPACE SCIENCES, 1962, 29 (01) :67-&
[7]   FREE WAVE PROPAGATION IN PERIODICALLY SUPPORTED, INFINITE BEAMS [J].
MEAD, DJ .
JOURNAL OF SOUND AND VIBRATION, 1970, 11 (02) :181-&
[9]   VIBRATION MEASUREMENTS OF AN AIRPLANE FUSELAGE STRUCTURE .1. TURBULENT BOUNDARY-LAYER EXCITATION [J].
WILBY, JF ;
GLOYNA, FL .
JOURNAL OF SOUND AND VIBRATION, 1972, 23 (04) :443-&
[10]  
WILBY JF, 1967, AFFDLTR6770 USAF REP