Accession Number:

ADA160736

Title:

The Test Loads Sequences Applied to the CT4 Full Scale Fatigue Test.

Descriptive Note:

Technical memo.,

Corporate Author:

AERONAUTICAL RESEARCH LABS MELBOURNE (AUSTRALIA)

Personal Author(s):

Report Date:

1985-06-01

Pagination or Media Count:

25.0

Abstract:

This document presents an outline of the derivation of the test load sequences applied to the CTA full scale fatigue test. Keywords Fatigue test Load sequence Aerodynamic loads Rare loads Gust loads LoadsForces CT-4 Aircraft Fatigue life Australia.

Subject Categories:

  • Aerodynamics

Distribution Statement:

APPROVED FOR PUBLIC RELEASE