Article contents
Mechanical Tests of Aircraft Structural Components
Published online by Cambridge University Press: 28 July 2016
Abstract
An abstract is not available for this content so a preview has been provided. Please use the Get access link above for information on how to access this content.
![Image of the first page of this content. For PDF version, please use the ‘Save PDF’ preceeding this image.'](https://static.cambridge.org/content/id/urn%3Acambridge.org%3Aid%3Aarticle%3AS0368393100113069/resource/name/firstPage-S0368393100113069a.jpg)
- Type
- Proceedings
- Information
- Copyright
- Copyright © Royal Aeronautical Society 1932
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
(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
- 2
- Cited by