| 000 -LEADER |
|---|
| fixed length control field |
00559pam a2200133a 44500 |
| 082 ## - DEWEY DECIMAL CLASSIFICATION NUMBER |
|---|
| Classification number |
NASA |
| Item number |
NEMO 1-27-59L |
| 100 ## - MAIN ENTRY--PERSONAL NAME |
|---|
| Personal name |
Gainer,Thomas G |
| 245 1# - TITLE STATEMENT |
|---|
| Title |
LOW-SPEED WIND-TUNNEL INVESTIGATION TO DETERMINE THE AERODYNAMIC CHARACTERISTICS OF A RECTANGULAR WING EQUIPPED WITH A FULL-SPAN AND AN INBOARD HALF-SPAN JET-AUGMENTED FLAP DEFLECTED 55 DEGREE |
| 260 ## - PUBLICATION, DISTRIBUTION, ETC. |
|---|
| Place of publication, distribution, etc. |
|
| Name of publisher, distributor, etc. |
Nasa, Washington, D.C. |
| Date of publication, distribution, etc. |
1959 |
| 300 ## - PHYSICAL DESCRIPTION |
|---|
| Extent |
21 |
| 500 ## - GENERAL NOTE |
|---|
| General note |
Bound With Nasa Memo 1-15-59l-26,30-31, Lack No.1-18-59l-1-19-59l,1-21-59l,1-28-59l-1-29-59l |
| 964 ## - |
|---|
| -- |
CIRC |
| 997 ## - |
|---|
| -- |
TR17741 C |
