Static and Fatigue Tests of F-111B Boron Wing Tip
Final rept. Jun-Dec 1969
AIR FORCE FLIGHT DYNAMICS LAB WRIGHT-PATTERSON AFB OH
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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.
- Attack and Fighter Aircraft
- Laminates and Composite Materials