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Theoretical prediction of thick wing and pylon-fuselage-fanpod-nacelle aerodynamic characteristics at subcritical speeds. part 2: computer program description
| Content Provider | NASA Technical Reports Server (NTRS) |
|---|---|
| Author | Kojima, J. Tulinius, J. R. |
| Copyright Year | 1974 |
| Description | The procedures required to operate the thick wing and pylon-fuselage-fanpod-nacelle computer program are presented. The program computes surface velocities and pressure, section loads, and total configuration loads and pitching moment. Potential flow theory is used to compute the surface pressures and the associated lift, moment, and vortex drag. The skin friction drag is also computed. |
| File Size | 9855176 |
| Page Count | 342 |
| File Format | |
| Alternate Webpage(s) | http://archive.org/details/NASA_NTRS_Archive_19750003864 |
| Archival Resource Key | ark:/13960/t8cg4gs0v |
| Language | English |
| Publisher Date | 1974-07-24 |
| Access Restriction | Open |
| Subject Keyword | Aircraft Design, Testing And Performance Body-wing Configurations Skin Friction Performance Prediction Aerodynamic Interference Flow Theory Data Processing Nacelles Aerodynamic Characteristics Pylons Computer Programs Wing Camber Ntrs Nasa Technical Reports ServerĀ (ntrs) Nasa Technical Reports Server Aerodynamics Aircraft Aerospace Engineering Aerospace Aeronautic Space Science |
| Content Type | Text |
| Resource Type | Technical Report |