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.

Subject Categories:

  • Aerodynamics
  • Statistics and Probability

Distribution Statement:

APPROVED FOR PUBLIC RELEASE