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
Descriptors:
Subject Categories:
- Aircraft
- Mechanics