Aerostructural Design and Its Application to Aluminum–Lithium Alloys
Authors:
- R.J.H. WanhillRWR.J.H. Wanhill
- G.H. BrayGBG.H. Bray
- 1 January 2014
- book chapter
- Published by Elsevier
- p. 27-58
Abstract
No abstract availableThis publication has 10 references indexed in Scilit:
- Low-energy intergranular fracture in Al–Li alloysEngineering Failure Analysis, 2012
- The Evolution of Al-Li Base Products for Aerospace and Space ApplicationsMetallurgical and Materials Transactions A, 2012
- The lead crack fatigue lifing frameworkInternational Journal of Fatigue, 2011
- Aluminum-Copper-Lithium Alloy 2050 Developed for Medium to Thick PlateJournal of Materials Engineering and Performance, 2009
- Progress in structural materials for aerospace systems11The Golden Jubilee Issue—Selected topics in Materials Science and Engineering: Past, Present and Future, edited by S. Suresh.Acta Materialia, 2003
- Mechanical behaviour of aluminium-lithium alloysSādhanā, 2003
- On the Effect of Thermomechanical Processing on the Mechanical Properties of 2297 PlatesMaterials Science Forum, 2002
- Application of modern aluminum alloys to aircraftProgress in Aerospace Sciences, 1996
- Status and prospects for aluminium-lithium alloys in aircraft structuresInternational Journal of Fatigue, 1994
- Mechanical properties of Al–Li alloys Part 1 Fracture toughness and microstructureMaterials Science and Technology, 1989