000 -LEADER |
fixed length control field |
00594pam a2200193a 44500 |
003 - CONTROL NUMBER IDENTIFIER |
control field |
OSt |
005 - DATE AND TIME OF LATEST TRANSACTION |
control field |
20210907110141.0 |
008 - FIXED-LENGTH DATA ELEMENTS--GENERAL INFORMATION |
fixed length control field |
210907b 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 |
082 ## - DEWEY DECIMAL CLASSIFICATION NUMBER |
Classification number |
NASA |
Item number |
TN D-1961 |
100 ## - MAIN ENTRY--AUTHOR NAME |
Personal name |
Shivers, James P. |
245 1# - TITLE STATEMENT |
Title |
Hovering characteristics of a rotor having an airfoil section designed for flying-crane type of helicopter |
Statement of responsibility, etc |
James P. Shivers |
260 ## - PUBLICATION, DISTRIBUTION, ETC. (IMPRINT) |
Place of publication |
Washington, D.C. |
Name of publisher |
NASA |
Year of publication |
1961 |
300 ## - PHYSICAL DESCRIPTION |
Number of Pages |
24p. |
500 ## - GENERAL NOTE |
General note |
Bound With Nasa Tn D741-746,748-50. |
650 ## - SUBJECT ADDED ENTRY--TOPICAL TERM |
Topical Term |
Aircraft stability and control |
942 ## - ADDED ENTRY ELEMENTS (KOHA) |
Koha item type |
Books |