Finite element elastic-plastic-creep and cyclic life analysis of a cowl lip /

Bibliographic Details
Main Author:	Arya, V. K., 1939-
Corporate Author:	United States. National Aeronautics and Space Administration
Other Authors:	Melis, Matthew E., Halford, Gary R.
Format:	Government Document Microform Book
Language:	English
Published:	[Washington, D.C.] : National Aeronautics and Space Administration, [1990]
Series:	NASA technical memorandum ; 102342.
Subjects:	Engine inlets. Finite element method. Leading edges. Life (Durability) Strain distribution. Stress distribution.
Online Access:	https://purl.fdlp.gov/GPO/LPS66083