学术探索
学术期刊
新闻热点
数据分析
智能评审

THEORETICAL AND EXPERIMENTAL PANEL FLUTTER STUDIES IN MACH NUMBER RANGE 1.0 TO 5.0

被引：80
作者：
DOWELL, EH
VOSS, HM
机构：
来源：
AIAA JOURNAL | 1965年 / 3卷 / 12期
关键词：
D O I：
10.2514/3.3359
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：2292 / &
相关论文
共 14 条
[1]   FLUTTER ANALYSIS OF FLAT RECTANGULAR PANELS BASED ON 3-DIMENSIONAL SUPERSONIC POTENTIAL FLOW [J].
CUNNINGHAM, HJ .
AIAA JOURNAL, 1963, 1 (08) :1795-1801
[2]   THE EFFECT OF A CAVITY ON PANEL VIBRATION [J].
DOWELL, EH ;
VOSS, HM .
AIAA JOURNAL, 1963, 1 (02) :476-476
[3]  
DOWELL EH, 1963, ASDTDR63449 TECHN DO
[4]   FLUTTER OF RECTANGULAR SIMPLY SUPPORTED PANELS AT HIGH SUPERSONIC SPEEDS [J].
HEDGEPETH, JM .
JOURNAL OF THE AERONAUTICAL SCIENCES, 1957, 24 (08) :563-&
[5]  
LOCK MH, 1961, TN670 US AIR FORC OF
[6]  
MCCLURE JD, 1962, AFOSR62187 US AIR FO
[7]  
MCCLURE JD, 1962, 622 FLUID DYN RES LA
[8]  
NELSON HC, 1955, NACATN3465
[9]  
SPIEGEL JM, 1956, NACARMA55121
[10]  
Warburton GB, 1954, P I MECH ENG A-J POW, V168, P371, DOI [10.1243/PIME_PROC_1954_168_040_02, DOI 10.1243/PIME]
12