Andere Kunden interessierten sich auch für
![A Systems Engineering Approach to Integrated Structural Health Monitoring for Aging Aircraft]( "A Systems Engineering Approach to Integrated Structural Health Monitoring for Aging Aircraft")
A Systems Engineering Approach to Integrated Structural Health Monitoring for Aging Aircraft61,99 €![Counterinsurgency Aircraft Procurement Options: Processes, Methods, Alternatives, and Estimates]( "Counterinsurgency Aircraft Procurement Options: Processes, Methods, Alternatives, and Estimates")
Counterinsurgency Aircraft Procurement Options: Processes, Methods, Alternatives, and Estimates60,99 €![BDA Enhancement Methodology Using Situational Parameter Adjustments]( "BDA Enhancement Methodology Using Situational Parameter Adjustments")
BDA Enhancement Methodology Using Situational Parameter Adjustments61,99 €![Cobol Reengineering Using the Parameter Based Object Identification Methodology]( "Cobol Reengineering Using the Parameter Based Object Identification Methodology")
Cobol Reengineering Using the Parameter Based Object Identification Methodology60,99 €![Electromagnetic Modeling and Measurement of Adaptive Metamaterial Structural Elements]( "Electromagnetic Modeling and Measurement of Adaptive Metamaterial Structural Elements")
Electromagnetic Modeling and Measurement of Adaptive Metamaterial Structural Elements60,99 €![Input Shaping to Reduce Solar Array Structural Vibrations]( "Input Shaping to Reduce Solar Array Structural Vibrations")
Input Shaping to Reduce Solar Array Structural Vibrations61,99 €![Conceptual Design Oriented Wing Structural Analysis and Optimization]( "Conceptual Design Oriented Wing Structural Analysis and Optimization")
Conceptual Design Oriented Wing Structural Analysis and Optimization60,99 €
The USAF initiated the Aircraft Structural Integrity Program (ASIP) over 40 years ago because of catastrophic, unanticipated, in-flight fatigue failures of in-service aircraft. In essence, ASIP is the management tool for the USAF to safely manage the fleet from initial operating capability through the design service goal and beyond. Since ASIP's inception, the USAF has not had a single catastrophic structural failure. The primary analysis tool to determine the fatigue life of a structural component in ASIP is linear elastic fracture mechanics (LEFM). In this effort, nine LEFM parameters were identified that affect the fatigue life: initial flaw assumption, boundary correction factor, load interaction models, crack growth rate data, stress intensity factor, threshold stress intensity factor, yield stress, and critical stress intensity factor.
Hinweis: Dieser Artikel kann nur an eine deutsche Lieferadresse ausgeliefert werden.
Hinweis: Dieser Artikel kann nur an eine deutsche Lieferadresse ausgeliefert werden.