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The jacobi matrix technique in computational fluid dynamics. ph.d. thesis
| Content Provider | NASA Technical Reports Server (NTRS) |
|---|---|
| Author | Sharp Sr., H. Thomas |
| Copyright Year | 1988 |
| Description | The Jacobi matrix technique was applied to the direct calculation of inviscid supersonic flow about two dimensional airfoils of varying thickness, angle of attack and camber and axisymmetric bodies of varying thickness and taper; and the design (inverse) calculation of inviscid supersonic flow past airfoils described by a given family of pressure distributions and axisymmetric bodies described by a given family of pressure distributions. The method was also applied to subsonic potential flow about two dimensional airfoils by modifying Jameson's FLO36. Results are discussed. |
| File Size | 1508733 |
| Page Count | 59 |
| File Format | |
| Alternate Webpage(s) | http://archive.org/details/NASA_NTRS_Archive_19870018915 |
| Archival Resource Key | ark:/13960/t7pp40c9m |
| Language | English |
| Publisher Date | 1988-05-01 |
| Access Restriction | Open |
| Subject Keyword | Numerical Analysis Supersonic Flow Boundary Value Problems Computational Fluid Dynamics Flow Distribution Jacobi Matrix Method Pressure Distribution Inviscid Flow Airfoils Two Dimensional Flow Rankine-hugoniot Relation Aerothermodynamics Ntrs Nasa Technical Reports Server (ntrs) Nasa Technical Reports Server Aerodynamics Aircraft Aerospace Engineering Aerospace Aeronautic Space Science |
| Content Type | Text |
| Resource Type | Thesis |
