Fatigue sensitivity analysis using complex variable methods

Author:

Voorhees A.,Millwater H.,Bagley R.,Golden P.

Publisher

Elsevier BV

Subject

Industrial and Manufacturing Engineering,Mechanical Engineering,Mechanics of Materials,General Materials Science,Modeling and Simulation

Reference25 articles.

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2. NASGROW fracture mechanics and fatigue crack growth analysis software, v6.0, NASA-JSC and Southwest Research Institute; 2009.

3. A new tool for design and certification of aircraft turbine rotors;Leverant;J Eng Gas Turbines Power,2004

4. McGinty RD. Sensitivity of fatigue crack growth rates to operating conditions, sample problem no. MERC-3. In: Miedlar PC, Berens AP, Gunderson AW, Gallagher JP, editors. USAF Damage Tolerant Design Handbook: Guidelines for the Analysis and Design of Damage Tolerant Aircraft Structures, AFRL-VA-WP-TR-2003-3002,Wright-Patterson Air Force Base, OH; November 2002 .

5. Fawaz SA, Harter JA. Impact of parameter accuracy on aircraft structural integrity estimates. US Air Force Technical Report, AFRL-VA-WPTR-2001-3057; 2001.

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