Loading...
Please wait, while we are loading the content...
Development of the learjet 28/29 wing using nastran analysis
| Content Provider | NASA Technical Reports Server (NTRS) |
|---|---|
| Author | Boroughs, R. R. |
| Copyright Year | 1980 |
| Description | 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. |
| File Size | 7529548 |
| Page Count | 22 |
| File Format | |
| Alternate Webpage(s) | http://archive.org/details/NASA_NTRS_Archive_19800016157 |
| Archival Resource Key | ark:/13960/t22c3tn9p |
| Language | English |
| Publisher Date | 1980-05-01 |
| Access Restriction | Open |
| Subject Keyword | Structural Mechanics Structural Design Weight Mass Bending Moments Lear Jet Aircraft Wings Aerodynamic Configurations Skin Structural Member Size Determination Nastran Ntrs Nasa Technical Reports Server (ntrs) Nasa Technical Reports Server Aerodynamics Aircraft Aerospace Engineering Aerospace Aeronautic Space Science |
| Content Type | Text |
| Resource Type | Article |
