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Direct calculation of airfoils from pressure distribution
| Content Provider | NASA Technical Reports Server (NTRS) |
|---|---|
| Author | Eppler, R. |
| Organization | The National Aeronautics and Space Administration (NASA) |
| Copyright Year | 1974 |
| Abstract | A method for determining airfoil profiles from the pressure or velocity distribution is described. The numerical factors make it possible to specify the profile thickness and to calculate the entire profile series by superposition. A minor disadvantage in the method is discussed and the procedure for correcting the discrepancy is analyzed. Mathematical models of the method are developed. The data for various types of airfoils are presented in graph form. |
| File Size | 2543384 |
| File Format | |
| Alternate Webpage(s) | http://www.archive.org/details/nasa_techdoc_19740011528 |
| Archival Resource Key | ark:/13960/t8ff4h68s |
| Language | English |
| Publisher Date | 1974-03-01 |
| Access Restriction | Open |
| Subject Keyword | Argon Plasma Gaseous Fission Reactors Plasma Diagnostics Radio Frequencies Electric Fields Magnetic Fields Magnetohydrodynamic Flow Plasma Heating Temperature Gradients Ntrs Nasa Technical Reports ServerĀ (ntrs) Nasa Technical Reports Server Aerodynamics Aircraft Aerospace Engineering Aerospace Aeronautic Space Science |
| Content Type | Text |