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Steels Used in Aero Work
Published online by Cambridge University Press: 24 August 2017
Extract
Before proceeding, I wish to say that I much appreciate the invitation to present this paper to your Society. The science of aeronautics has evolved at a great pace, and typifies what can be done with applied science, and the tangible results are so apparent that it would be superfluous to discuss them. It would .appear to me that the rapidity with which the efficiency has increased is due to the whole-hearted collaboration of the different branches of applied science and engineering, the honours being shared, after giving first place to the sporting instinct of the early flyer, by the physicist, the engineer, and the metallurgist. You will notice that my modesty places the metallurgist last. It is quite a confession to make, but it is a fact, nevertheless, that I accepted with pleasure your invitation to give this paper, principally because I have always taken a keen interest in the metallurgical side of aeronautics.
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- Copyright © Royal Aeronautical Society 1917
References
Note on page 259 * The factor of strength as fixed by the authorities is well known to be so many times the "oad borne by the supporting surfaces during straight horizontal flight.
Note on page 260 * Stanton & Bairstow, Proc. Inst. C.E., 1906, Vol. CIXVI.
Note on page 262 * Institution of Automobile Engineers, November, 1915.
Note on page 263 † Burls, p. 137, Aero Engines.
Note on page 263 * P. Breuil.
Note on page 263 * A Martens, "Materialienkunde fur den Maschinenbau."
Note on page 268 * Un win's Testing of Materials.
Note on page 285 * McWilliam and Barnes.
Note on page 288 * Noted by Professor Hopkinson in 1859.
Note on page 288 † Invar and Related Nickel Steels."
Note on page 291 * Institution of Automobile Engineers, 1915.
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