Minimum cost and weight design of fuselage frames
Author:
- Christos KassapoglouCKChristos Kassapoglou
- 1 July 1999
- journal article
- Published by Elsevier in Composites Part A: Applied Science and Manufacturing
- Vol. 30 (7) , 887-894
Abstract
No abstract availableKeywords
This publication has 4 references indexed in Scilit:
- Minimum cost and weight design of fuselage frames: Part B: cost considerations, optimization, and resultsComposites Part A: Applied Science and Manufacturing, 1999
- Simultaneous cost and weight minimization of composite-stiffened panels under compression and shearComposites Part A: Applied Science and Manufacturing, 1997
- The use of COSTADE in developing composite commercial aircraft fuselage structures1994
- The Crippling Strength of Compression ElementsJournal of the Aerospace Sciences, 1958