NASA NTRS · 19800016157
Development of the Learjet 28/29 Wing Using NASTRAN Analysis
Abstract
The 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.
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Boroughs, R. R.. 1980-05-01. Development of the Learjet 28/29 Wing Using NASTRAN Analysis. https://ntrs.nasa.gov/citations/19800016157
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