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On the calculation of flow about objects traveling at high supersonic speeds
| Content Provider | NASA Technical Reports Server (NTRS) |
|---|---|
| Copyright Year | 1952 |
| Description | A procedure for calculating three-dimensional steady and nonsteady supersonic flows with the method of characteristics is developed and discussed. An approximate method is deduced from the characteristics method and shown to be of practical value at high supersonic speeds. |
| File Size | 1380513 |
| Page Count | 26 |
| File Format | |
| Alternate Webpage(s) | http://archive.org/details/NASA_NTRS_Archive_19930083552 |
| Archival Resource Key | ark:/13960/t8w99hp8m |
| Language | English |
| Publisher Date | 1952-10-01 |
| Access Restriction | Open |
| Subject Keyword | Bodies Wings Flow, Supersonic Airplanes Aerodynamics, Fundamental Missiles 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 |
