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Supersonic flow past nonlifting bumped and indented bodies of revolution
| Content Provider | NASA Technical Reports Server (NTRS) |
|---|---|
| Copyright Year | 1956 |
| Description | Linear-theory values of the supersonic pressure field and wave drag of nonlifting bumped and indented bodies of revolution are presented and compared with the corresponding properties of a smooth body. The comparisons indicate that relatively small surface irregularities cause large pressure disturbances and changes in wave drag. The interference drag produced by bumps and indentations is discussed and a correction for the curvature of the characteristics is applied. |
| File Size | 1205890 |
| Page Count | 40 |
| File Format | |
| Alternate Webpage(s) | http://archive.org/details/NASA_NTRS_Archive_19930084560 |
| Archival Resource Key | ark:/13960/t0zp8rm7z |
| Language | English |
| Publisher Date | 1956-09-01 |
| Access Restriction | Open |
| Subject Keyword | Flow, Supersonic Bodies - Shape Variables Bodies - Aerodynamic Theory 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 |