Fatigue methodology III; Proceedings of the AHS National Technical Specialists' Meeting on Advanced Rotorcraft Structures, Scottsdale, AZ, Oct. 3-5, 1989
Papers on rotorcraft and fatigue methodology are presented, covering topics such as reliability design for rotorcraft, a comparison between theory and fatigue test data on stress concentration factors, the retirement lives of rolling element bearings, hydrogen embrittlement risk analysis for high hardness steel parts, and rotating system load monitoring with minimum fixed system instrumentation. Additional topics include usage data collection to improve structural integrity of operational helicopters, usage monitory of military helicopters, improvements to the fatigue substantiation of the H-60 composite tail rotor blade, helicopter surviellance programs, and potential application of automotive fatigue technology in rotorcraft design. Also, consideration is given to fatigue evaluation of C/MH-53 E main rotor damper threaded joints, SH-2F airframe fatigue test program, a ply termination concept for improving fracture and fatigue strength of composite laminates, the analysis and testing of composite panels subject to muzzle blast effects, the certification plan for an all-composite main rotor flexbeam, and the effects of stacking sequence on the flexural strength of composite beams.
- OSTI ID:
- 6600547
- Report Number(s):
- CONF-8910448-
- Resource Relation:
- Conference: AHS national technical specialists' meeting on advanced rotocraft structures, Scottsdale, AZ (USA), 3-5 Oct 1989
- Country of Publication:
- United States
- Language:
- English
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Related Subjects
36 MATERIALS SCIENCE
AIRCRAFT COMPONENTS
FATIGUE
HELICOPTERS
DESIGN
COMPOSITE MATERIALS
HARDNESS
HYDROGEN EMBRITTLEMENT
JOINTS
LEADING ABSTRACT
MATERIALS
MEETINGS
METALS
MILITARY EQUIPMENT
ORIENTATION
RELIABILITY
ROLLER BEARINGS
ROTORS
STEELS
ABSTRACTS
AIRCRAFT
ALLOYS
BEARINGS
DOCUMENT TYPES
ELEMENTS
EMBRITTLEMENT
EQUIPMENT
IRON ALLOYS
IRON BASE ALLOYS
MECHANICAL PROPERTIES
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