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 :
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