Reliability-Based Structural Design of a Representative Wing and Tail System Together with Structural Tests-Reference-Cited by-同舟云学术

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Reliability-Based Structural Design of a Representative Wing and Tail System Together with Structural Tests

Published:2011-04-04 Issue: Volume: Page:
ISSN:
Container-title:52nd AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics and Materials Conference
language:
Short-container-title:

Author:

Acar Erdem¹

Affiliation:

1. TOBB ETU

Publisher

American Institute of Aeronautics and Astronautics

Link

http://arc.aiaa.org/doi/pdf/10.2514/6.2011-1761

Reference39 articles.

1. Lincoln, J.W. "Method for Computation of Structural Failure Probability for an Aircraft," ASD-TR-80-5035, Wright-PattersonAFB,OH,July1980.

2. Shiao,M.C.,Nagpal,V.K.,and Chamis,C.C."Probabilistic Structural Analysis of Aerospace ComponentsUsingNESSUS," AIAA 88-2373,1988.

3. Wirsching, P.H. "Literature Review on Mechanical Reliability and Probabilistic Design," Probabilistic Structural Analysis MethodsforSelectSpacePropulsion SystemComponents(PSAM),NASACR189159,Vol. III,1992.

4. Lykins, C., Thomson, D., and Pomfret, C. "The Air Force's Application of Probabilistics to Gas Turbine Engines," AIAA94-1440-CP,1994.

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