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Heat transfer and pressure distributions on hemisphere-cylinders in methane-air combustion products at mach 7
| Content Provider | NASA Technical Reports Server (NTRS) |
|---|---|
| Author | Weinstein, I. |
| Copyright Year | 1973 |
| Description | Heat-transfer and pressure distributions were measured over the surfaces of three hemisphere-cylinder models tested at a nominal Mach number of 7 in the Langley 8-foot high-temperature structures tunnel which uses methane-air products of combustion as a test medium. The results showed that the heat-transfer and pressure distributions over the surface of the models were in good agreement with experimental data obtained in air and also with theoretical predictions. |
| File Size | 7693079 |
| Page Count | 41 |
| File Format | |
| Alternate Webpage(s) | http://archive.org/details/NASA_NTRS_Archive_19730006198 |
| Archival Resource Key | ark:/13960/t7wm6227c |
| Language | English |
| Publisher Date | 1973-01-01 |
| Access Restriction | Open |
| Subject Keyword | Thermodynamics And Combustion Methane Combustion Physics Hypersonic Speed Cylindrical Bodies Pressure Distribution Wind Tunnel Apparatus Wind Tunnel Models Test Equipment Heat Transfer Aerothermodynamics Hemispherical Shells 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 |
