DocumentCode
966015
Title
A Method of Preliminary Aeroelastic Stability Analysis
Author
Frain, W.E. ; Wong, B.
Author_Institution
John Hopkins University, Baltimore
Volume
6
Issue
3
fYear
1962
fDate
9/1/1962 12:00:00 AM
Firstpage
18
Lastpage
28
Abstract
This paper determines natural frequencies, responses and mode shapes used to calculate dynamic environmental inputs to electronic and electromechanical equipment in a missile,
Keywords
Accelerometers; Actuators; Aerodynamics; Filters; Frequency; Missiles; Servomechanisms; Shape; Stability analysis; Tail;
fLanguage
English
Journal_Title
Product Engineering and Production, IRE Transactions on
Publisher
ieee
ISSN
0096-1760
Type
jour
DOI
10.1109/TPEP.1962.1136308
Filename
1136308
Link To Document