Papers by Author: David J. Chellman

Paper TitlePage

Evaluation of AA 2050-T87 Al-Li Alloy Crack Turning Behaviour
Authors: Matthew J. Crill, David J. Chellman, Ed S. Balmuth, Mike Philbrook, K. Paul Smith, Alex Cho, Michael Niedzinski, Raphael Muzzolini, Jim Feiger
Abstract: Crack turning or delamination behavior of AA 2050-T87 and AA 7050-T7451 ESE(T) and hourglass coupons under cyclic fatigue conditions is presented. Fatigue crack growth rate curves, fracture surface examinations, and the preferred manner of crack growth for each alloy are discussed in an effort to better understand fatigue crack growth behavior of aluminum-lithium alloys in structural components under service conditions.
1323
Comparison of the Thermal-Mechanical Stability of Three Al-Cu-Mg-X Alloys
Authors: M.A. Cantrell, T.D. Bayha, David J. Chellman, D.L. Yaney
1777
Aerospace Applications of Advanced Aluminum Alloys
Authors: David J. Chellman, S.L. Langenbeck
49
Deformation Behavior and Properties of Mechanically Alloyed Aluminum Alloys
Authors: J.H. Weber, David J. Chellman
221
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