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 :
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