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Mechanical Tests of Aircraft Structural Components

Published online by Cambridge University Press:  28 July 2016

I. J. Gerard
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Type
Proceedings
Information
The Aeronautical Journal , Volume 36 , Issue 261 , September 1932 , pp. 673 - 703
Copyright
Copyright © Royal Aeronautical Society 1932

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References

(1) “Protection of Metal Parts of Aircraft against Corrosion.” Sutton. Royal Aeronautical Society Journal, January, 1932.Google Scholar
(2) “A Method of Testing the Strength of Aircraft Hulls.” Gerard. R. and M. 1398, November, 1930.Google Scholar
(3) “Mechanical Testing in Aircraft Construction.” Gerard. Royal Aeronautical Society Journal, July, 1931.Google Scholar
(4) “An Analysis of Some Causes of Discrepancy between the Calculated Failing Load of the Structure of an Aircraft and the Load at which Failure occurs on Strength Test.” Howard and Spencer. R. and M. 1125, August, 1927. Cf. I.C.A.N. Official Bulletin No. 7, §9 of Resolution No. 182.Google Scholar
(5) “Dynamische Bruchversuche mit Flugzengbauteilen.” Hertel. D.V.L., Jahrbuch, 1931.Google Scholar
(6) “The Pressure Distribution over the Wings and Tail Surfaces of a PW-9 Pursuit Airplane in Flight.” Rhode. N.A.C.A. Report No. 364, 1930.Google Scholar
Cf. Report of the Scale Effect Sub-Committee on the Relation between Model Tests and the Full Scale Performance of Aeroplanes. R. and M. 374, December, 1917.Google Scholar
(7) “Aufzeichnen schneller Schwingungen nach dem Ritzverfahren.” Pabst. D.V.L., Jahrbuch, 1930.Google Scholar