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A computer program for two-dimensional and axisymmetric nonreacting perfect gas and equilibrium chemically reacting laminar, transitional and-or turbulent boundary layer flows
| Content Provider | NASA Technical Reports Server (NTRS) |
|---|---|
| Author | Miner, E. W. Lewis, C. H. Anderson, E. C. |
| Copyright Year | 1971 |
| Description | A computer program is described in detail for laminar, transitional, and/or turbulent boundary-layer flows of non-reacting (perfect gas) and reacting gas mixtures in chemical equilibrium. An implicit finite difference scheme was developed for both two dimensional and axisymmetric flows over bodies, and in rocket nozzles and hypervelocity wind tunnel nozzles. The program, program subroutines, variables, and input and output data are described. Also included is the output from a sample calculation of fully developed turbulent, perfect gas flow over a flat plate. Input data coding forms and a FORTRAN source listing of the program are included. A method is discussed for obtaining thermodynamic and transport property data which are required to perform boundary-layer calculations for reacting gases in chemical equilibrium. |
| File Size | 8524698 |
| Page Count | 190 |
| File Format | |
| Alternate Webpage(s) | http://archive.org/details/NASA_NTRS_Archive_19750013915 |
| Archival Resource Key | ark:/13960/t44r2nm2c |
| Language | English |
| Publisher Date | 1971-05-01 |
| Access Restriction | Open |
| Subject Keyword | Computer Programming And Software Rocket Nozzles Chemical Equilibrium Laminar Boundary Layer Finite Difference Theory Turbulent Boundary Layer Ideal Gas Wind Tunnel Nozzles Two Dimensional Flow Computer Programs Fortran Axisymmetric Flow 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 |
