Title :
A Method of Preliminary Aeroelastic Stability Analysis
Author :
Frain, W.E. ; Wong, B.
Author_Institution :
John Hopkins University, Baltimore
fDate :
9/1/1962 12:00:00 AM
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;
Journal_Title :
Product Engineering and Production, IRE Transactions on
DOI :
10.1109/TPEP.1962.1136308