| 000 -LEADER |
|---|
| fixed length control field |
00601nam a2200169 4500 |
| 005 - DATE AND TIME OF LATEST TRANSACTION |
|---|
| control field |
20200527153222.0 |
| 008 - FIXED-LENGTH DATA ELEMENTS--GENERAL INFORMATION |
|---|
| fixed length control field |
200527b 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 |
NACA |
| Item number |
TN-2882 |
| 100 ## - MAIN ENTRY--AUTHOR NAME |
|---|
| Personal name |
Stokes, Fred H. |
| 245 ## - TITLE STATEMENT |
|---|
| Title |
Theoretical investigation of the longitudinal response characteristics of a swept-wing fighter airplane having a pitch-attitude control system |
| Statement of responsibility, etc |
Fred, H. Stokes and J. T. Matthews |
| 260 ## - PUBLICATION, DISTRIBUTION, ETC. (IMPRINT) |
|---|
| Place of publication |
Washington, D. C. |
| Name of publisher |
National Advisory Committee for Aeronautics |
| Year of publication |
1953 |
| 300 ## - PHYSICAL DESCRIPTION |
|---|
| Number of Pages |
41p |
| 700 ## - ADDED ENTRY--PERSONAL NAME |
|---|
| Personal name |
Matthews, J. T. |
| 942 ## - ADDED ENTRY ELEMENTS (KOHA) |
|---|
| Koha item type |
Books |
