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Analysis and design of three dimensional supersonic nozzles. volume 2: numerical program for analysis of nozzle-exhaust flow fields
| Content Provider | NASA Technical Reports Server (NTRS) |
|---|---|
| Author | Kalben, P. |
| Copyright Year | 1972 |
| Description | The FORTRAN IV Program developed to analyze the flow field associated with scramjet exhaust systems is presented. The instructions for preparing input and interpreting output are described. The program analyzes steady three dimensional supersonic flow by the reference plane characteristic technique. The governing equations and numerical techniques employed are presented in Volume 1 of this report. |
| File Size | 7028356 |
| Page Count | 173 |
| File Format | |
| Alternate Webpage(s) | http://archive.org/details/NASA_NTRS_Archive_19740003001 |
| Archival Resource Key | ark:/13960/t71w08q8k |
| Language | English |
| Publisher Date | 1972-10-01 |
| Access Restriction | Open |
| Subject Keyword | Fluid Mechanics Supersonic Flow Flow Equations Nozzle Design Numerical Analysis Nozzle Flow Supersonic Nozzles Flow Distribution Flow Geometry Computer Programs Fortran 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 |