000 -LEADER |
fixed length control field |
00611nam a22001817a 4500 |
003 - CONTROL NUMBER IDENTIFIER |
control field |
OSt |
005 - DATE AND TIME OF LATEST TRANSACTION |
control field |
20210315111418.0 |
008 - FIXED-LENGTH DATA ELEMENTS--GENERAL INFORMATION |
fixed length control field |
210315b 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 |
Kremzier, Email J. |
245 ## - TITLE STATEMENT |
Title |
A method for evaluating the effects of drag and inlet pressure recovery on propulsion system performance [ Technical Note 3261 ] |
Statement of responsibility, etc |
Email J. Kremzier |
260 ## - PUBLICATION, DISTRIBUTION, ETC. (IMPRINT) |
Place of publication |
Washington |
Name of publisher |
National Advisory committee for Aeronautics |
Year of publication |
1954 |
300 ## - PHYSICAL DESCRIPTION |
Number of Pages |
21p |
440 ## - SERIES STATEMENT/ADDED ENTRY--TITLE |
Title |
National Advisory committee for Aeronautics (NACA) |
650 ## - SUBJECT ADDED ENTRY--TOPICAL TERM |
Topical Term |
Pressure |
942 ## - ADDED ENTRY ELEMENTS (KOHA) |
Koha item type |
Reference |