DocumentCode
1369995
Title
Study of aircraft cooling systems for rotating electric equipment
Author
Martin, G. Cecil
Author_Institution
Jack and Heintz, Inc., Cleveland, Ohio
Volume
71
Issue
3
fYear
1952
fDate
7/1/1952 12:00:00 AM
Firstpage
150
Lastpage
160
Abstract
THE steadily increasing upper limits in flight speed and altitude for modern aircraft are making the study of rotating electric equipment cooling systems imperative. Experience with conventional fan and blast cooling systems indicates poor cooling performance under many of the high-altitude, high-speed flight conditions now being encountered. Further, there are strong indications that other types of cooling may extract a lower over-all penalty from the airplane than the conventional systems.
Keywords
Airplanes; Cooling; Equations; Generators; Heat transfer; Ocean temperature;
fLanguage
English
Journal_Title
American Institute of Electrical Engineers, Part II: Applications and Industry, Transactions of the
Publisher
ieee
ISSN
0097-2185
Type
jour
DOI
10.1109/TAI.1952.6371217
Filename
6371217
Link To Document