| 000 -LEADER |
|---|
| fixed length control field |
00437pam a2200145a 44500 |
| 082 ## - DEWEY DECIMAL CLASSIFICATION NUMBER |
|---|
| Classification number |
NACA |
| Item number |
TM-1420 |
| 100 ## - MAIN ENTRY--PERSONAL NAME |
|---|
| Personal name |
Corcos,G M |
| 245 1# - TITLE STATEMENT |
|---|
| Title |
ON THE CONTRIBUTION OF TURBULENT BOUNDARY LAYERS TO THE NOISE INSIDE A FUSELAGE |
| 260 ## - PUBLICATION, DISTRIBUTION, ETC. |
|---|
| Place of publication, distribution, etc. |
|
| Name of publisher, distributor, etc. |
National Advisory Committee For Aeronautics, Washington,D.C. |
| Date of publication, distribution, etc. |
1956 |
| 300 ## - PHYSICAL DESCRIPTION |
|---|
| Extent |
43 |
| 500 ## - GENERAL NOTE |
|---|
| General note |
Bound With Naca Tm-1421-1429. |
| 700 ## - ADDED ENTRY--PERSONAL NAME |
|---|
| Personal name |
Liepmann,H W |
| 964 ## - |
|---|
| -- |
CIRC |
| 997 ## - |
|---|
| -- |
17288 C |
