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Explicit expression to predict the erosive burning rate of solid propellants
| Content Provider | NASA Technical Reports Server (NTRS) |
|---|---|
| Author | Wang, S. |
| Copyright Year | 1986 |
| Description | Using the theory of gas dynamics and heat transfer from a turbulent gas flow to the burning surface of propellant along a permeable wall, an explicit expression is derived to predict the burning rate of the solid propellant with crossflow. Results of the calculation have been compared with experimental data and proved to be correct. |
| File Size | 4472003 |
| Page Count | 9 |
| File Format | |
| Alternate Webpage(s) | http://archive.org/details/NASA_NTRS_Archive_19860018787 |
| Archival Resource Key | ark:/13960/t3rv5fh02 |
| Language | English |
| Publisher Date | 1986-07-01 |
| Access Restriction | Open |
| Subject Keyword | Propellants And Fuels Turbulent Flow Gas Flow Predictions Solid Propellants Permeability Walls Heat Transfer Cross Flow Burning Rate Erosive Burning Ntrs Nasa Technical Reports Server (ntrs) Nasa Technical Reports Server Aerodynamics Aircraft Aerospace Engineering Aerospace Aeronautic Space Science |
| Content Type | Text |
| Resource Type | Article |
