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First Frederik J Plantema Memorial Lecturethe International
Reliability analysis based on time to the first failure
Design and certification for executive type aircraft
16 other sections not shown
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acceleration Aeronaut agricultural aircraft aircraft structure airframe airline airplane alloys altitude analysis applied Aviation bending bolt calculated cent coefficient of variation components corrosion cost crack propagation cumulative frequency cycles damage effect elements engine evaluation experience extreme value distribution fail-safe structure fail-safe tests failure fastener fatigue cracks fatigue load fatigue test flap Flight Data Recorder flight load flying hours frequency distribution function fuselage Gust velocity helicopter ICAF increase increments inspection installation load factor load spectrum load transfer loading segment main rotor maneuvers material measured method normal obtained operations panels plate pressure probability problem ratio record reduced reduction factors reliability rigid rotor safe-life shot peened shown in Fig skin spar specimens spectra speed steel stiffened straingauge stress concentration stringer supersonic transport surface tail rotor take-off temperature test results thermal stresses titanium transport ultimate load undercarriage weight wing