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Transonic perturbation analysis of wing-fuselage-nacelle-pylon configurations with powered jet exhausts
| Content Provider | NASA Technical Reports Server (NTRS) |
|---|---|
| Author | Wai, J. C. Yoshihara, H. Sun, C. C. |
| Copyright Year | 1982 |
| Description | A method using a transonic small disturbance code with successive line over-relaxation is described for treating wing/fuselage configurations with a nacelle/pylon/powered jet. Examples illustrating its use for the NASA transport research model are given. Reasonable test/theory comparisons were obtained. |
| File Size | 1391145 |
| Page Count | 69 |
| File Format | |
| Alternate Webpage(s) | http://archive.org/details/NASA_NTRS_Archive_19820011293 |
| Archival Resource Key | ark:/13960/t7tn22206 |
| Language | English |
| Publisher Date | 1982-02-01 |
| Access Restriction | Open |
| Subject Keyword | Aerodynamics Transonic Flow Body-wing Configurations Jet Impingement Finite Difference Theory Coordinates Pressure Distribution Wing Nacelle Configurations Mathematical Models Upper Surface Blowing Pylons Ntrs Nasa Technical Reports ServerĀ (ntrs) Nasa Technical Reports Server Aircraft Aerospace Engineering Aerospace Aeronautic Space Science |
| Content Type | Text |
| Resource Type | Technical Report |