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A solution of the direct and inverse potential problems for arbitrary cascades of airfoils
| Content Provider | NASA Technical Reports Server (NTRS) |
|---|---|
| Copyright Year | 1944 |
| Description | Methods are given of determining the potential flow plast an arbitrary cascade of airfoils and the inverse problem of determining an airfoil having a prescribed velocity distribution in cascade. Results indicated that Cartesian mapping function method may be satisfactorily extended to include cascades. Numerical calculation for computing cascades by Cartesian mapping function method is considerably greater than for single airfoils but much less than hitherto required for cascades. Detailed results are presented graphically. |
| File Size | 1944127 |
| Page Count | 51 |
| File Format | |
| Alternate Webpage(s) | http://archive.org/details/NASA_NTRS_Archive_19930092715 |
| Archival Resource Key | ark:/13960/t1vf0227d |
| Language | English |
| Publisher Date | 1944-01-01 |
| Access Restriction | Open |
| Subject Keyword | Pressure Distribution - Airfoils Airfoils - Cascades Theories - Conformal Transformation Airfoils - Circular Transformation Cartesian Mapping 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 |
