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First derivatives of flow quantities behind two-dimensional, nonuniform supersonic flow over a convex corner. ph.d. thesis - george washington univ.
| Content Provider | NASA Technical Reports Server (NTRS) |
|---|---|
| Author | Darden, C. M. |
| Copyright Year | 1985 |
| Description | A method of determining spatial derivatives of flow quantities behind an expansion fan as a function of the curvature of the streamline behind the fan is developed. Taylor series expansions of flow quantities within the fan are used and boundary conditions satisfied to the first and second order so that the curvature of the characteristics in the fan may be determined. A system of linear equations for the spatial derivatives is then developed. An application of the method to shock coalescence including asymmetric effects is described. |
| File Size | 638984 |
| Page Count | 20 |
| File Format | |
| Alternate Webpage(s) | http://archive.org/details/NASA_NTRS_Archive_19850008519 |
| Archival Resource Key | ark:/13960/t6d26t15x |
| Language | English |
| Publisher Date | 1985-01-01 |
| Access Restriction | Open |
| Subject Keyword | Aerodynamics Supersonic Flow Coalescing Extrapolation Nonuniform Flow Shock Waves Corner Flow Series Expansion Taylor Series Linear Equations Curvature Ntrs Nasa Technical Reports Server (ntrs) Nasa Technical Reports Server Aircraft Aerospace Engineering Aerospace Aeronautic Space Science |
| Content Type | Text |
| Resource Type | Thesis |
