Accession Number:

ADA018751

Title:

Static and Fatigue Tests of F-111B Boron Wing Tip

Descriptive Note:

Final rept. Jun-Dec 1969

Corporate Author:

AIR FORCE FLIGHT DYNAMICS LAB WRIGHT-PATTERSON AFB OH

Personal Author(s):

Report Date:

1975-06-01

Pagination or Media Count:

42.0

Abstract:

This report describes the structural integrity tests of the F-111B boron-epoxy wing tip. A single test specimen was subjected to static load tests, static load plus internal pressure in the fuel cell tests, a fatigue test simulating four service lifetimes and residual strength tests. Results are discussed.

Subject Categories:

  • Attack and Fighter Aircraft
  • Laminates and Composite Materials

Distribution Statement:

APPROVED FOR PUBLIC RELEASE