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Material Trends in the United Kingdom for Structure Operating at Temperatures up to 700 F (380C)
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Kiddle, P. and McKenzie, P., "Material Trends in the United Kingdom for Structure Operating at Temperatures up to 700 F (380C)," SAE Technical Paper 620536, 1962, https://doi.org/10.4271/620536.Also In
References
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- Doyle W. M. How I. M. Glanville Jones R. “Extrapolation on Long-Term Data From Room and Elevated Temperature Tensile Results on Hiduminium 66 Clad Sheet to B. S. L73.” High Duty Alloys Report SX. 4941.
- Hayward D. C. “The Mechanical Properties of RR 58 Aluminium Alloy Sheet (Clad) in Tension and Compression at Room and Elevated Temperatures.” Royal Aircraft Establishment Tech. Note Met. 261
- Doyle W. M. “Structural Aluminum Alloys for High Speed Flight.” Journal of Royal Aeronautical Society September 1960
- Imperial Chemical Industries published data on titanium and titanium alloys.
- A. V. Roe Ltd. Miscellaneous data.
- Firth Vickers Ltd. Private communication J. Morley.
- F. V. 520 Firth Vickers semi-austenitic precipitation hardening steel.
- Jessop-Saville Ltd. English Steel Corp., United Steel Co. Ltd. Miscellaneous data.
- Work on 5% Cr-Mo-V Steel (H. 50, vacuum melted Jessop Saville Ltd). De Havilland Aircraft Co. Ltd. Central Materials Laboratory.
- Wilkinson F. J. Cottrell C. L. M. “Rocket-Motor Cases.” “Factors Affecting the Use of High-Strength Steels.” Aircraft Production August and September 1960
- Based on data and information supplied by the Royal Aircraft Establishment Farnborough, U.K