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Enhancement of the cave computer code. [aerodynamic heating package for nose cones and scramjet engine sidewalls]
| Content Provider | NASA Technical Reports Server (NTRS) |
|---|---|
| Author | Rathjen, K. A. Burk, H. O. |
| Copyright Year | 1983 |
| Description | The computer code CAVE (Conduction Analysis via Eigenvalues) is a convenient and efficient computer code for predicting two dimensional temperature histories within thermal protection systems for hypersonic vehicles. The capabilities of CAVE were enhanced by incorporation of the following features into the code: real gas effects in the aerodynamic heating predictions, geometry and aerodynamic heating package for analyses of cone shaped bodies, input option to change from laminar to turbulent heating predictions on leading edges, modification to account for reduction in adiabatic wall temperature with increase in leading sweep, geometry package for two dimensional scramjet engine sidewall, with an option for heat transfer to external and internal surfaces, print out modification to provide tables of select temperatures for plotting and storage, and modifications to the radiation calculation procedure to eliminate temperature oscillations induced by high heating rates. These new features are described. |
| File Size | 3931597 |
| Page Count | 85 |
| File Format | |
| Alternate Webpage(s) | http://archive.org/details/NASA_NTRS_Archive_19840005433 |
| Archival Resource Key | ark:/13960/t9r25s77q |
| Language | English |
| Publisher Date | 1983-12-01 |
| Access Restriction | Open |
| Subject Keyword | Fluid Mechanics And Heat Transfer Wall Temperature Temperature Distribution Thermal Protection Supersonic Combustion Ramjet Engines Aerodynamic Heating Eigenvalues Nose Cones Blunt Bodies Computerized Simulation Leading Edges Heat Transfer Hypersonic Vehicles 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 |