Accession Number:
ADA250341
Title:
Reduction and Analysis of F-111C Flight Data.
Descriptive Note:
Technical memo,
Corporate Author:
AERONAUTICAL RESEARCH LABS MELBOURNE (AUSTRALIA)
Personal Author(s):
Report Date:
1991-12-01
Pagination or Media Count:
51.0
Abstract:
As part of a programme to determine inspection intervals for the stiffener runout regions of the upper plates of the wing pivot fittings of RAAF F-111 aircraft, the possible influence on crack growth of stores carried and of low and negative g-spectrum loading has been examined for reconnaissance aircraft, the remaining F-111 fleet and for aircraft A8-148. Derived gust loading spectra for the same F-111 groups have also been determined. F-111C wing pivot fittings, Fatigue crack growth, Exceedences, Gust loads, F-111C aircraft.
Descriptors:
Subject Categories:
- Aerodynamics
- Statistics and Probability