Reduction and Analysis of F-111C Flight Data.

Piperias, P.

Reduction and Analysis of F-111C Flight Data.

Active / Technical Report | Accession Number: ADA250341 |

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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.

Author(s):

Piperias, P.

Author Organization(s):

AERONAUTICAL RESEARCH LABS MELBOURNE (AUSTRALIA)

Descriptive Note:

Technical memo,

Pagination:

0051

Security Markings

DOCUMENT & CONTEXTUAL SUMMARY

Distribution:

Approved For Public Release

RECORD

Collection: TR

Identifying Numbers

Report Number(s):

ARL-STRUC-TM-544, DODA-AR-006-633

Monitor Series:

AR-006-633

Subject Terms

Joint Capability Areas:

JCA_6.3.3_Spectrum Management

Communities of Interest:

Air Platforms

Descriptor(s):

*STATISTICAL ANALYSIS, *DATA REDUCTION, *FLIGHT LOADS, AIRCRAFT, CRACKS, FATIGUE, FITTINGS, GUST LOADS, GUSTS, INSPECTION, INTERVALS, PIVOTS, PLATES, RECONNAISSANCE, RECONNAISSANCE AIRCRAFT, REGIONS, SPECTRA, STORES, WINGS, CRACK PROPAGATION, GROWTH(GENERAL), AUSTRALIA

Field(s)/Group(s):

Aerodynamics, Statistics and Probability

Keyword(s):

F 111 C Aircraft

Report Date:

1991 Dec 01