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Calculation of transonic flows past thin airfoils by integral method
| Content Provider | NASA Technical Reports Server (NTRS) |
|---|---|
| Copyright Year | 1950 |
| File Size | 4366779 |
| Page Count | 98 |
| File Format | |
| Alternate Webpage(s) | http://archive.org/details/NASA_NTRS_Archive_19930082753 |
| Archival Resource Key | ark:/13960/t6m08fp7s |
| Language | English |
| Publisher Date | 1950-07-01 |
| Access Restriction | Open |
| Subject Keyword | Flow Velocity, High - Transonic Flow Velocity - Distribution Theories - Airfoils - Thin Flow - Shock Waves Airfoils, Biconvex Airfoils, Symmetrical Flow - Airfoils Compressible (2-dimensional) Theories - Flow - Transonic Airfoils - Thickness 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 |