000 -LEADER |
fixed length control field |
00628pam a2200193a 44500 |
008 - FIXED-LENGTH DATA ELEMENTS--GENERAL INFORMATION |
fixed length control field |
160408b1978 xxu||||| |||| 00| 0 eng d |
082 ## - DEWEY DECIMAL CLASSIFICATION NUMBER |
Classification number |
629.1323 |
Item number |
W831e |
100 ## - MAIN ENTRY--PERSONAL NAME |
Personal name |
Wolf, Thomas L. |
245 1# - TITLE STATEMENT |
Title |
EFFECT OF TIP VORTEX STRUCTURE OF HELICOPTER NOISE DUE TO BLADE |
Statement of responsibility, etc. |
VORTEX INTERACTION ; REPORT |
260 ## - PUBLICATION, DISTRIBUTION, ETC. |
Place of publication, distribution, etc. |
Massachusetts |
Name of publisher, distributor, etc. |
Institute Of Technology |
Date of publication, distribution, etc. |
1978 |
300 ## - PHYSICAL DESCRIPTION |
Extent |
94 |
440 ## - SERIES STATEMENT/ADDED ENTRY--TITLE |
Title |
Nasa-Cr-152150, M. I. T. Fluid Dynamics Research Laboratory Report |
Volume/sequential designation |
78-2 |
650 ## - SUBJECT ADDED ENTRY--TOPICAL TERM |
Topical term or geographic name entry element |
Aerodynamic Noise |
650 ## - SUBJECT ADDED ENTRY--TOPICAL TERM |
Topical term or geographic name entry element |
Helicopters |
650 ## - SUBJECT ADDED ENTRY--TOPICAL TERM |
Topical term or geographic name entry element |
Vortex-Motion |
700 ## - ADDED ENTRY--PERSONAL NAME |
Personal name |
Windall, Sheila E. |
964 ## - |
-- |
CIRC |
997 ## - |
-- |
A77730 C |