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Evaluation of the Heat Dissipated inside Compartments by Internal Structural Members on High Speed Aircraft

Published online by Cambridge University Press:  04 July 2016

R. Le Claire
R. Le Claire*
Affiliation:
Hawker Siddeley Aviation Limited, Kingston-on-Thames
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Extract

This note deals with an extension of the basic fin theory, as found in refs. 1 and 2, suitably modified to estimate the heat dissipated by internal structure such as consoles, floors, bulkheads, and so on. It also outlines the electrical analogy method applied to complex structures.

Type
Technical Notes
Information
The Aeronautical Journal , Volume 70 , Issue 664 , April 1966 , pp. 534 - 537
Copyright
Copyright © Royal Aeronautical Society 1966

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References

1.Jakob, M.Heat transfer. John Wiley & Sons. 5th Edition 1956.Google Scholar
2.Torgeson, W. L., Johnson, H. C. and Wright, N. B. Jnr, Engineering Study of Air Conditioning Load. Requirements for Aircraft Compartments. WADC Report 55-254. June 1955.Google Scholar
3.Applied Thermodynamics Manual, Society of Automotive Engineers, 1960.Google Scholar
4.Robinson, H. G. R. An Analogue Computer for Convective Heating. RAE, Tech Note No. GW434. October 1956.Google Scholar
5.Mcnaughton, I. I., Hughes, T. L. and Fielding, D. W. A Study of the Thermal Properties of Aircraft Cabin Insulation using Electrical Analogue Technique. RAE, Tech Note Mech Eng 351. April 1962.Google Scholar