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The Metalclad Airship
Published online by Cambridge University Press: 28 July 2016
Extract
An invitation to address the Royal Aeronautical Society, the first Society of its kind ever founded, is indeed a signal honour and not without misgivings to a humble visitor who, in the land of Elizabethan English, finds himself embarrassed for words adequate to express his appreciation. The scientific contribution of the Society to the advancement of aeronautics and the meritorious achievements of its members are well known in the United States.
A sort of unselfish and patient willingness, which encourages men to depart from beaten paths and invade unknown realms to bring forth something new and beneficial to society, is indispensable to any new enterprise, and most characteristic of those who are pioneers in airship development. Certainly none so far have garnered any substantial profits.
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References
2 F.R.Ae.S., Chief Designer of ZMC-2, Professor Aeronautical Engineering, University of Michigan; awarded Wright Brothers Medal, 1930.
3 Through the co-operation of Mr. C. F. Kettering, Director, General Motors Research Laboratories, and Mr. W. B. Mayo, Chief Engineer of Ford Motor Company (both of whom are members of the Technical Committee of Aircraft Development Corporation).
4 Also Consulting Engineer to the U.S. Navy on Submarine and Airship Design.
5 Also Consulting Engineer to the U.S. Shipping Board.
6 Acknowledgment is gratefully expressed for the unfailing co-operation of the Bureau of Aeronautics of the U.S. Navy, for whom the ship was built, and to various membersof the personnel of the National Advisory Committee for Aeronautics and of the Bureau of Standards, who extended invaluable scientific aid.
7 More complete description contained in “Aircraft Engineering,” London, Vol. II., No. 6, June, 1930, page 148; and in “Transactions of A.S.M.E.” Aer., Vol. 51, January–April, 1930, pages 245-266.
8 Aluminium Company of America, 17 St.
9 Scientific contribution of E. H. Dix, Jr., and C. F. Nagel, of Aluminium Company of America, and of Dr. E. Blough, Chief of Research, Aluminium, Limited.
10 Aeronautical Engineer, U.S. Navy; R.Ae.S. commended R.38 Memorial Prize Paper submitted in 1923 jointly by Mr. Burgess, Comdr. J. C. Hunsaker, U.S.N., and Mr. Starr Truscott on “ The Strength of Rigid Airships.”
11 Research Engineer, Bureau of Standards.
Note on page 844 * R.100: The weight empty of the R.100 has been taken as 86 tons, in accordance with Mr. Wallis’ statement in his lecture before the Royal Aeronautical Society, May 10th, 1928 (see “ Aircraft Engineering,” January, 1930, page 10). In the absence of any definite information the ton has been considered as metric (2,200 lbs.).
12 J. S. McDonnel, Jr., in “Airway Age,” February, 1931, based on analysis for 1925 by Dr. Carl Pirath.
13 Hon.F.R.Ae.S., formerly Naval Attaché, American Embassy in London; Vice–President Goodyear–Zeppelin Corporation.
14 Recent announcements of discoveries of helium in the Mackenzie River Valley, Canada, and in the Belgian Congo, confirm this prediction.
Note on page 857 * By W. A. Klikofi, Aeronautical Engineer, Aircraft Development Corporation, Detroit, Mich. Presented at the National Meeting of the A.S.M.E., Aeronautic Division, in Baltimore, May 14, 1931, and reprinted here through the courtesy of Mr. Klikoff and the American Society of Mechanical Engineers.
Note on page 860 * Technical Report §325 National Advisory Committee for Aeronautics.
Note on page 861 * R. H. Upson's paper, “ Metalclad Rigid Airship Development,” delivered before the S.A.E., February, 1926, gives the original ideas on internal pressure control as applied to Metalclad airships.
Note on page 872 * “The Development of Rigid Airship Construction” by Lieut.-Col. V. C. Richmond, O.B.E., B.Sc. ; the Paper was read before the British Association, at Bristol, on September 8th, 1930.
Note on page 875 * Quoted from “Zeitschrift fur Flugtechnik und Motorluftschiffahrt,” December 29, 1930, page 630.
Note on page 879 * Trans. A.S.M.E. January–April, 1928, AER–6.