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Some Approximate Formulae for Transient Temperature Prediction in Aircraft-Type Structures

Published online by Cambridge University Press:  04 July 2016

D. J. Johns  and
M. J. Wooldridge
D. J. Johns
Affiliation:
Loughborough University of Technology
M. J. Wooldridge
Affiliation:
Hawker Siddeley Dynamics (Coventry)
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Extract

The solution of the general heat transfer problem for typical aircraft-type structures usually involves a finite element approach involving the solution of a large number of simultaneous equations. This may be performed by calculation using a digital computer or with an analogue simulator. For calculations involving both spatial and time intervals considerable care must be exercised to obtain solutions which are not divergent or oscillatory and this usually involves very small time increments and a large total computation time.

Type
Technical Notes
Information
The Aeronautical Journal , Volume 71 , Issue 675 , March 1967 , pp. 223 - 226
Copyright
Copyright © Royal Aeronautical Society 1967

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References

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