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The Effects of Kinetic Heating on Aircraft Structures*

Published online by Cambridge University Press:  04 July 2016

A. W. Kitchenside
A. W. Kitchenside*
Affiliation:
formerly Guided Weapons Department, now Aircraft Project Office, Vickers-Armstrongs (Aircraft) Ltd.
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Extract

Kinetic heating, which is associated with supersonic flight, is probably the greatest challenge which has confronted the structural engineer, since the design and analysis of affected structures requires a radical extension of current practice. For example, the laws of heat transfer and the effects of high temperature on structural materials become important factors in structural analysis. To obtain a clear appreciation of the situation it is therefore necessary for the designers of the structure to become familiar with these factors, together with certain aspects of boundary layer theory.

Type
Research Article
Information
The Aeronautical Journal , Volume 62 , Issue 566 , February 1958 , pp. 105 - 117
Copyright
Copyright © Royal Aeronautical Society 1958

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Footnotes

*

A lecture given to the Graduates' and Students' Section of the Society on 23rd November 1956.

References

1.Monaghan, R. J. Formulae and Approximations for Aerodynamic Heating Rates in High Speed Flight. Unpublished R.A.E. Report.Google Scholar
2.Eckert, E. R. G. Survey on Heat Transfer at High Speeds. W.A.D.C. Tech. Rep. 54–70.Google Scholar
3.Davies, F. V. and Monaghan, R. J. The Estimation of Skin Temperature attained in High Speed Flight. Unpublished R.A.E. Report.Google Scholar
4.Schuh, H. (1954). On the Calculation of Temperature Distribution and Thermal Stresses in Parts of Supersonic Aircraft. Journal of the Aeronautical Sciences, August 1954.Google Scholar
5.Hoff, N. J. (1956). Comparison of Radiant and Convective Heat Transfer in a Supersonic Wing. Journal of the Aeronautical Sciences, July 1956.Google Scholar
6.Bisplinghoff, R. L. (1956). Some Structural and Aeroelastic Considerations of High Speed Flight. Journal of the Aeronautical Sciences, April 1956.Google Scholar
7.Willoughby, G. Interim Report on the Mechanical Properties of Fully Heat Treated Hiduminium RR58 Clad Sheet at Room and Elevated Temperature. High Duty Alloys Research Division Report SX 4359.Google Scholar
8.Willoughby, G. Mechanical Properties of Hiduminium RR58, Part V. Creep Properties. High Duty Alloys Research Division Report SX4368.Google Scholar
9. Hiduminium 100. High Duty Alloys Brochure.Google Scholar
10. Meikle, G. Summary of the Effects of Heating Some Aluminium Alloys and Alloy Steels at Elevated Temperatures. Unpublished R.A.E. Report.Google Scholar
11.Hughes, P. J., Inge, J. E. and Prosser, S. B. Tensile and Compressive Stress—Strain Properties of Some High Strength Sheet Alloys at Elevated Temperatures. N.A.C.A. T.N. 3315.Google Scholar
12.Binning, M. S. and Ballet, J. T. Mechanical Properties of Titanium Alloy. R.C. C-110M and Ti 140A. Unpublished R.A.E. Report.Google Scholar
13. The Engineering Properties of Commercial Titanium Alloys. Titanium Metallurgical Laboratory, Battelle Memorial Institute. T.M.L. Rep. No. 15.Google Scholar
14. Armco Precipitation Hardening Stainless Steels. Armco Steel Corporation Brochure.Google Scholar
15. Hylite Titanium Alloys. William Jessop and Sons Ltd. BrochureGoogle Scholar
16. Wrought Titanium. Imperial Chemical Industries Ltd. Brochure.Google Scholar
17.Flanigan, A. E., Tedsen, L. F. and Dorn, J. E.Compressive Properties of Aluminium Alloy Sheet at Elevated Temperatures. A.S.T.M., Vol. 46, pp. 951–967.Google Scholar
18.Heimerl, G. J. and Barrett, P. F. A Structural Efficiency Evaluation of Titanium at Normal and Elevated Temperatures. N.A.C.A. T.N. 2269.Google Scholar
19.Catchpole, E. J. (1954). The Optimum Design of Compression Surfaces having Unflanged Integral Stiffeners. Journal of the Royal Aeronautical Society, November 1954.Google Scholar
20.Farrar, D. J. (1949). The Design of Compression Structures for Minimum Weight. Journal of the Royal Aeronautical Society, p. 1041, November 1949.CrossRefGoogle Scholar
21.Mathauser, E. E. and Deveikis, W. D. Investigation of the Compressive Strength and Creep Lifetime of 2024-T3 Aluminium Alloy Plates at Elevated Temperatures. N.A.C.A. T.N. 3552.Google Scholar
22.Hoff, N. J. (1956). Creep Buckling. Aeronautical Quarterly, February 1956.CrossRefGoogle Scholar
23.Hoff, N. J. (1955). Rapid Creep in Structures. Journal of the Aeronautical Sciences, October 1955.CrossRefGoogle Scholar
24.Parkes, E. W. (1953). Transient Thermal Stresses in Wings. Aircraft Engineering, December 1953.CrossRefGoogle Scholar
25.Goldberg, M. A. (1956). Investigation of the Temperature Distribution and Thermal Stresses in a Hypersonic Wing Structure. Journal of the Aeronautical Sciences, November 1956.CrossRefGoogle Scholar
26.Budiansky, B. and Mayers, J. (1956). Influence of Aerodynamic Heating on the Effective Torsional Stiffness of Thin Wings. Journal of the Aeronautical Sciences, December 1956.CrossRefGoogle Scholar
27.Griffiths, G. E. and Miltonberger, G. M. Some Effects of Joint Conductivity on the Temperatures and Thermal Stresses in Aerodynamically Heated Skin Stiffener Combinations. N.A.C.A. T.N. 3699.Google Scholar
28.Heldenfels, R. R. The Effect of Non-Uniform Temperature Distributions on the Strength and Distortions of Stiffened-Shell Structures. N.A.C.A. T.N. 2240.Google Scholar
29.Fung, Y. C. (1954). The Static Stability of a Two-Dimensional Curved Panel in a Supersonic Flow with an Application to Panel Flutter. Journal of the Aeronautical Sciences, August 1954.CrossRefGoogle Scholar
30.Argyris, J. H. and Kelsey, S. (1954). Energy Theorems and Structural Analysis, Part II. Aircraft Engineering, December 1954.Google Scholar
31.Gerard, G. (1954). Life Expectancy of Aircraft under Thermal Flight. Journal of the Aeronautical Sciences, October 1954.CrossRefGoogle Scholar
32.Horton, W. H. (1954). Laboratory Simulation of Kinetic Heating. Aircraft Engineering, May 1954.CrossRefGoogle Scholar
33.McLellan, G. H. Melting of Bodies due to Aerodynamic Heating. A.S.M.E. Paper 54-A-157.Google Scholar