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Computer program for definition of transonic axial-flow compressor blade rows
| Content Provider | NASA Technical Reports Server (NTRS) |
|---|---|
| Author | Crouse, J. E. |
| Copyright Year | 1975 |
| Description | Particular type of blade element used has two segments which have centerlines and surfaces described by constant change of angle with path distance on cone. Program is result of rework of earlier program to give major gains in accuracy, reliability and speed. It also covers more steps of overall compressor design procedure. |
| File Size | 91251 |
| Page Count | 1 |
| File Format | |
| Alternate Webpage(s) | http://archive.org/details/NASA_NTRS_Archive_19750000021 |
| Archival Resource Key | ark:/13960/t1dk06m5m |
| Language | English |
| Publisher Date | 1975-04-01 |
| Access Restriction | Open |
| Subject Keyword | Mathematics And Information Sciences Turbocompressors Axial Flow Turbines Compressor Blades Ibm 7090 Computer Ibm 7094 Computer Ibm 360 Computer Fortran 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 |