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A study of the motion and aerodynamic heating of missiles entering the earth's atmosphere at high supersonic speedsA simplified analysis of the velocity and deceleration history of missiles entering the earth's atmosphere at high supersonic speeds is presented. The results of this motion analysis are employed to indicate means available to the designer for minimizing aerodynamic heating. The heating problem considered involves not only the total heat transferred to a missile by convection, but also the maximum average and local time rates of convective heat transfer.
Document ID
19930084817
Acquisition Source
Legacy CDMS
Document Type
Other - NACA Technical Note
Authors
Allen, Julian H
Eggers, A J , Jr
Date Acquired
August 16, 2013
Publication Date
October 1, 1957
Subject Category
Aerodynamics
Report/Patent Number
NACA-TN-4047
Accession Number
93R14107
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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