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DETERMINATION OF FRACTURE TOUGHNESS FOR WHISKER-REINFORCED ALUMINIUM ALLOY MATRIX COMPOSITE USING CHEVRON-NOTCHED SPECIMEN.

Authors: Kazumi Hirano
Abstract:
American Society of Mechanical Engineers : Fairfield, New Jersey

Pages: 226
Report Date: 01 JAN 1991
Report Number: D306164

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Keywords relating to this report:
AIRFRAMES
CAPTIVE TESTS
COMPRESSORS
COOLING
DUCTED FANS
ENGINEERING
EXPERIMENTAL DATA
FLIGHT CONTROL SYSTEMS
FLIGHT TESTING
GRAPHICS
HANDLING
HEAT TRANSFER
HOVERING
LANDING GEAR
MANEUVERABILITY
MANUFACTURING
MODEL TESTS
NOSE WHEELS
PERFORMANCE(ENGINEERING)
RELIABILITY
RESEARCH AIRCRAFT
RESEARCH MANAGEMENT
SIMULATION
STABILITY
STALLING
TAILS(AIRCRAFT)
TEMPERATUREZ
TEMPERATUREZSTABILITY
TURBOJET ENGINES
WIND TUNNEL MODELS
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