INTERIOR NOISE RADIATED BY AN AIRPLANE FUSELAGE SUBJECTED TO TURBULENT BOUNDARY LAYER EXCITATION AND EVALUATION OF NOISE REDUCTION TREATMENTS

被引：22
作者：
BHAT, WV
WILBY, JF
机构：
来源：
JOURNAL OF SOUND AND VIBRATION | 1971年 / 18卷 / 04期
关键词：
D O I：
10.1016/0022-460X(71)90097-6
中图分类号：
O42 [声学];
学科分类号：
070206 ; 082403 ;
摘要：
引用
收藏
页码：449 / &
相关论文
共 13 条
[1]  
Beranek L., 1960, NOISE REDUCTION
[2]   FLIGHT TEST MEASUREMENT OF EXTERIOR TURBULENT BOUNDARY LAYER PRESSURE FLUCTUATIONS ON BOEING-MODEL-737 AIRPLANE [J].
BHAT, WV .
JOURNAL OF SOUND AND VIBRATION, 1971, 14 (04) :439-&
[3]  
KIRK JJ, 1966, T63572 BOEING TEST R
[4]  
LUDWIG GR, 1962, 87 U TOR I AER REP
[5]  
Lyon RH., 1967, RANDOM NOISE VIBRATI
[6]   MEASUREMENT OF NOISE RADIATED BY BOUNDARY LAYER EXCITED PANELS [J].
MAESTRELLO, L .
JOURNAL OF SOUND AND VIBRATION, 1965, 2 (02) :100-+
[7]  
MAESTRELLO L, 1964, D69944 BOEING DOC, V3
[8]  
MAESTRELLO L, 1964, D69944 BOEING DOC, V1
[9]  
MAESTRELLO L, 1964, D69944 BOEING DOC, V2
[10]  
MAESTRELLO L, 1968, J AIRCRAFT, V5, P321
12