DTIC ADA1050341: Effect of Fighter Attack Spectrum pdf

DTIC ADA1050341: Effect of Fighter Attack Spectrum

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Description of the Book:

The objective was to evaluate the effect of fighter wing load spectrum variations on the life behavior of composite structures. Six types of spectra were generated: (a) clipping to 90% test limit stress, (b) addition of stress overloads, (c) addition of low loads, (d) truncation to 70% test limit stress, (e) clipping of tension loads, (f) increased severity and number of air-to-air loads. A single hole compression test specimen was designed to simulate fatigue critical areas of fighter wing skins. (Author

• Creator/s: Badaliance,R
• Date: 3/1/1981
• Book Topics/Themes: DTIC Archive, Badaliance, R, MCDONNELL AIRCRAFT CO ST LOUIS MO, *COMPOSITE MATERIALS, *FATIGUE(MECHANICS), STRESSES, MATHEMATICAL MODELS, FIGHTER AIRCRAFT, LOADS(FORCES), GRAPHITE, SPECTRA, EPOXY LAMINATES, WINGS

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