| 000 -LEADER |
|---|
| fixed length control field |
00685nam a2200193 4500 |
| 005 - DATE AND TIME OF LATEST TRANSACTION |
|---|
| control field |
20200810102828.0 |
| 008 - FIXED-LENGTH DATA ELEMENTS--GENERAL INFORMATION |
|---|
| fixed length control field |
200810b 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 |
Wilbur, D. Middleton |
| 245 ## - TITLE STATEMENT |
|---|
| Title |
A numerical method for calculating the flat-plate pressure distribution on supersonic wings of supersonic wings of arbitrary planform. [NASA TN D-2570] |
| Statement of responsibility, etc |
Wilbur D. Middleton and Harry W. Carlson |
| 260 ## - PUBLICATION, DISTRIBUTION, ETC. (IMPRINT) |
|---|
| Place of publication |
Washington, D. C |
| Name of publisher |
NASA |
| Year of publication |
1965 |
| 300 ## - PHYSICAL DESCRIPTION |
|---|
| Number of Pages |
23p |
| 440 ## - SERIES STATEMENT/ADDED ENTRY--TITLE |
|---|
| Title |
National Aeronautics and Space Administration (NASA) |
| 505 ## - FORMATTED CONTENTS NOTE |
|---|
| Formatted contents note |
NASA technical report |
| 650 ## - SUBJECT ADDED ENTRY--TOPICAL TERM |
|---|
| Topical Term |
Arbitrary |
| 700 ## - ADDED ENTRY--PERSONAL NAME |
|---|
| Personal name |
Carlson, Harry W. |
| 942 ## - ADDED ENTRY ELEMENTS (KOHA) |
|---|
| Koha item type |
Technical Report |
