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Development of the Learjet 28/29 Wing Using NASTRAN AnalysisThe structural development work performed on the Learjet 28/29 wing using NASTRAN analysis is discussed. The work included the basic sizing of primary structural members such as wing skins, wing skin splices, and spar caps, as well as the calculation of preliminary weight estimates utilizing the weight computation routine in NASTRAN. The eight spar redundancy of the Learjet wing made this task somewhat more complex than for more determinate type wing structures. Some of the problems that were encountered and the solutions and methods that were used are described.
Document ID
19800016157
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Boroughs, R. R. (Gates Learjet Corp. Wichita, KS, United States)
Date Acquired
August 10, 2013
Publication Date
May 1, 1980
Publication Information
Publication: NASA. Goddard Space Flight Center Eighth NASTRAN User's Colloq.
Subject Category
Structural Mechanics
Accession Number
80N24650
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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IDRelationTitle19800016155Collected WorksEighth NASTRAN User's Colloquium
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