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Nastran analysis for the airmass sunburst model 'c' ultralight aircraft
| Content Provider | NASA Technical Reports Server (NTRS) |
|---|---|
| Author | Verbestel, John Smith, Howard W. |
| Copyright Year | 1993 |
| Description | The purpose of this project was to create a three dimensional NASTRAN model of the Airmass Sunburst Ultralight comparable to one made for finite element analysis. A two dimensional sample problem will be calculated by hand and by NASTRAN to make sure that NASTRAN finds similar results. A three dimensional model, similar to the one analyzed by the finite element program, will be run on NASTRAN. A comparison will be done between the NASTRAN results and the finite element program results. This study will deal mainly with the aerodynamic loads on the wing and surrounding support structure at an attack angle of 10 degrees. |
| File Size | 805590 |
| Page Count | 32 |
| File Format | |
| Alternate Webpage(s) | http://archive.org/details/NASA_NTRS_Archive_19930020588 |
| Archival Resource Key | ark:/13960/t9091621m |
| Language | English |
| Publisher Date | 1993-01-01 |
| Access Restriction | Open |
| Subject Keyword | Structural Mechanics Finite Element Method Wings Ultralight Aircraft Angle of Attack Nastran Three Dimensional Models Aerodynamic Loads Ntrs Nasa Technical Reports Server (ntrs) Nasa Technical Reports Server Aerodynamics Aircraft Aerospace Engineering Aerospace Aeronautic Space Science |
| Content Type | Text |
| Resource Type | Technical Report |
