NASA Logo

NTRS

NTRS - NASA Technical Reports Server

Back to Results
Analysis of the Learjet 35/36 Wing and Correlation with Experimental ResultsTwo NASTRAN models of the Gates Learjet Corporation Model 35/36 Wing were developed. The models and the problems encountered in their development are discussed. A skin buckling analysis used for the ultimate loading conditions is presented. A discussion of the static tests and the correlation of the static test with the NASTRAN results and the results of a supplementary semimonocoque beam analysis are also included.
Document ID
19770013558
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Abla, M. H.
(Gates Learjet Corp. Denver, CO, United States)
Boroughs, R. R.
(Gates Learjet Corp. Denver, CO, United States)
Cook, E. L.
(Wichita State Univ.)
Date Acquired
August 8, 2013
Publication Date
October 1, 1976
Publication Information
Publication: NASA. Ames Res. Center NASTRAN: User's Experiences
Subject Category
Structural Mechanics
Accession Number
77N20502
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
No Preview Available