| 000 -LEADER |
|---|
| fixed length control field |
00425pam a2200145a 44500 |
| 082 ## - DEWEY DECIMAL CLASSIFICATION NUMBER |
|---|
| Classification number |
TR |
| Item number |
COA-14 |
| 100 ## - MAIN ENTRY--PERSONAL NAME |
|---|
| Personal name |
Nonweiler,T. |
| 245 1# - TITLE STATEMENT |
|---|
| Title |
WAVE DRAG OF HIGHLY SEWPT WINGS |
| Statement of responsibility, etc. |
A COMPARISON OF LINEAR THEORY AND SLENDER BODY THEORY |
| 260 ## - PUBLICATION, DISTRIBUTION, ETC. |
|---|
| Place of publication, distribution, etc. |
|
| Name of publisher, distributor, etc. |
College Of Aeronautics, Cranfield |
| Date of publication, distribution, etc. |
1954 |
| 300 ## - PHYSICAL DESCRIPTION |
|---|
| Extent |
14 |
| 440 ## - SERIES STATEMENT/ADDED ENTRY--TITLE |
|---|
| Title |
College Of Aeronautics |
| Volume/sequential designation |
No.14 |
| 500 ## - GENERAL NOTE |
|---|
| General note |
Bound With: Coa 5-65 |
| 964 ## - |
|---|
| -- |
CIRC |
| 997 ## - |
|---|
| -- |
TR3023 C |
