Prediction of axial-flow instabilities in a turbojet engine by use of a multistage compressor simulation on the digital computer [ NASA TM X-3134] (Record no. 564460)
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| 000 -LEADER | |
|---|---|
| fixed length control field | 00575nam a2200145 4500 |
| 003 - CONTROL NUMBER IDENTIFIER | |
| control field | OSt |
| 040 ## - CATALOGING SOURCE | |
| Transcribing agency | IIT Kanpur |
| 041 ## - LANGUAGE CODE | |
| Language code of text/sound track or separate title | eng |
| 245 ## - TITLE STATEMENT | |
| Title | Prediction of axial-flow instabilities in a turbojet engine by use of a multistage compressor simulation on the digital computer [ NASA TM X-3134] |
| Statement of responsibility, etc | Carl J. Daniele, Ronald J.Blaha and Kurt Seldner |
| 260 ## - PUBLICATION, DISTRIBUTION, ETC. (IMPRINT) | |
| Place of publication | Washington D.C. |
| Name of publisher | National Aeronaticsand Space Administration |
| Year of publication | 1975 |
| 300 ## - PHYSICAL DESCRIPTION | |
| Number of Pages | 34p |
| 440 ## - SERIES STATEMENT/ADDED ENTRY--TITLE | |
| Title | National Aeronaticsand Space Administration (NASA) |
| 700 ## - ADDED ENTRY--PERSONAL NAME | |
| Personal name | Blaha,Ronald. J. and Seldner, Kurt |
| 942 ## - ADDED ENTRY ELEMENTS (KOHA) | |
| Koha item type | Books |
No items available.