Problems discussed for periods covering pre-1945 and 1945-55; safe life of spars; for immediate future, full scale and ad hoc testing of wings and cabins, and probably tailplanes is necessary; ultimate solution lies in design of structure, fatigue failure of which would be well beyond operational life. 2nd Barnwell Memorial Lecture. (See also Roy Aeronautical Soc -- J v 59 n 533 May 1955 p 339-48; Aeroplane v 88 n 2278 Mar 18 1955 p 357-9)
Outlook on airframe fatigue
Flight
Flight ; 67 , n 2408
1955
Article (Journal)
English
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