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AFML-TR-77-102, TECHNICAL REPORT: EXPLORATORY DEVELOPMENT FOR DESIGN DATA ON STRUCTURAL ALUMINUM ALLOYS IN REPRESENTATIVE AIRCRAFT ENVIRONMENTS (JUL-1977)

AFML-TR-77-102, TECHNICAL REPORT: EXPLORATORY DEVELOPMENT FOR DESIGN DATA ON STRUCTURAL ALUMINUM ALLOYS IN REPRESENTATIVE AIRCRAFT ENVIRONMENTS (JUL-1977)., The mechanical properties, fracture toughness, fatigue, fatigue-crack growth rates in three environments and corrosion characteristics of 10 lots each of 20148-T851, 7050-T7351 and 7475-T7351 plate and 2219-T852 hand forgings have been evaluated. Data for establishing MIL-HDBK-5 values, including modulus of elasticity and stress-strain are presented.

TR-77-102 Rev. 1977

    
 Status:
Active

 FSC Code:
 1560 - Airframe Structural Components

Version:
197707-19779.61 MB AFML-TR-77-102

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