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Radome thermal stress investigationComputer determinations of convergent series and continuous functions in main-body thermal stress solution for radomes of interceptor missiles during hypersonic flight
Document ID
19670024040
Acquisition Source
Legacy CDMS
Document Type
Other
Authors
Tate, M. B.
Date Acquired
August 3, 2013
Publication Date
March 1, 1967
Subject Category
Structural Mechanics
Accession Number
67N33369
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Keywords
HYPERSONIC FLIGHT
GUIDED MISSILE
THERMAL STRESS
CONTINUOUS FUNCTION
RADOME
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