Accession Number:

AD0669415

Title:

FATIGUE TEST RESULTS AND ANALYSIS OF FOUR PISTON PROVOST WINGS TESTED IN AN ASCENDING-DESCENDING ORDER OF LOADING,

Descriptive Note:

Corporate Author:

BRITISH AIRCRAFT CORP LTD LONDON (ENGLAND)

Personal Author(s):

Report Date:

1968-03-01

Pagination or Media Count:

12.0

Abstract:

Results of fatigue tests on four wings programme loaded in Lo-Hi-Lo order are compared with similar tests performed in Hi-Lo and Lo-Hi orders reported previously. The results lie almost mid-way between the results for Hi-Lo and Lo-Hi tests. No significant difference is shown in either the variance or mean value since the results lie within the scatter of the previous tests. Author

Subject Categories:

  • Aircraft
  • Mechanics

Distribution Statement:

APPROVED FOR PUBLIC RELEASE