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Volume 6, Issue 11
1 November 1934
This article was originally published in
Aircraft Engineering
Aircraft Engineering Cover Image for Volume 6, Issue 11
Review Article| November 01 1934

Static Wing‐Rib Tests: A Method of Calculating Approximate Values for the Loads to be Applied Available to Purchase

A.W. Clegg, B.Sc. A.F.R.Ae.S.
A.W. Clegg, B.Sc. A.F.R.Ae.S.
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Author & Article Information
Publisher: Emerald Publishing
Online ISSN: 2059-9366
Print ISSN: 0002-2667
© MCB UP Limited
1934
Aircraft Engineering (1934) 6 (11): 301.
https://doi.org/10.1108/eb029871

THE strength of main plane ribs for use on all British aircraft is determined by static tests of single representative ribs under conditions of loading determined from the characteristics of the aerofoil.

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© MCB UP Limited
1934
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