Oxidation and thermal fatigue cracking of nickel and cobalt base alloys in a high velocity gas stream [NASA TN D-5376] (Record no. 566393)
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| 000 -LEADER | |
|---|---|
| fixed length control field | 00698nam a22002057a 4500 |
| 003 - CONTROL NUMBER IDENTIFIER | |
| control field | OSt |
| 005 - DATE AND TIME OF LATEST TRANSACTION | |
| control field | 20230110161910.0 |
| 008 - FIXED-LENGTH DATA ELEMENTS--GENERAL INFORMATION | |
| fixed length control field | 230110b xxu||||| |||| 00| 0 eng d |
| 040 ## - CATALOGING SOURCE | |
| Transcribing agency | IIT Kanpur |
| 041 ## - LANGUAGE CODE | |
| Language code of text/sound track or separate title | eng |
| 100 ## - MAIN ENTRY--AUTHOR NAME | |
| Personal name | Johnston, James R. |
| 245 ## - TITLE STATEMENT | |
| Title | Oxidation and thermal fatigue cracking of nickel and cobalt base alloys in a high velocity gas stream [NASA TN D-5376] |
| Statement of responsibility, etc | James R. Johnston |
| 260 ## - PUBLICATION, DISTRIBUTION, ETC. (IMPRINT) | |
| Place of publication | Washington, D. C. |
| Name of publisher | National Aeronautics and Space Administration |
| Year of publication | 1969 |
| 300 ## - PHYSICAL DESCRIPTION | |
| Number of Pages | 48p |
| 440 ## - SERIES STATEMENT/ADDED ENTRY--TITLE | |
| Title | National Aeronautics and Space Administration |
| 440 ## - SERIES STATEMENT/ADDED ENTRY--TITLE | |
| Title | NASA Technical Note |
| 500 ## - GENERAL NOTE | |
| General note | Bound vol. contains NASA TN D 5371-5380 |
| 650 ## - SUBJECT ADDED ENTRY--TOPICAL TERM | |
| Topical Term | Gas stream |
| 942 ## - ADDED ENTRY ELEMENTS (KOHA) | |
| Koha item type | Technical Report |
| Withdrawn status | Lost status | Damaged status | Not for loan | Collection code | Home library | Current library | Date acquired | Serial Enumeration / chronology | Accession Number | Koha item type |
|---|---|---|---|---|---|---|---|---|---|---|
| COMPACT STORAGE (BASEMENT) | PK Kelkar Library, IIT Kanpur | PK Kelkar Library, IIT Kanpur | 10/01/2023 | NASA TN D 5371-5380 | TR009340 | Technical Report |