DocumentCode
1370599
Title
Altitude chamber requirements for evaluating blast-cooled aircraft generators
Author
Scott, H. Dale
Author_Institution
Naval Research Laboratory, Washington, D. C.
Volume
71
Issue
6
fYear
1953
Firstpage
427
Lastpage
430
Abstract
ALTITUDE chambers have proved beneficial in the development of equipment to be installed in aircraft. By determining the conditions under which the equipment is to be operated and then simulating those conditions in altitude chambers, it has been possible to discover deficiencies and make corrections prior to installation of the equipment in aircraft. This procedure has made it possible to complete the development programs on the auxiliary equipment so that flight-test emphasis has been on the overall performance of the aircraft. Aircraft performance has been aided materially by the use of altitude chambers.
Keywords
Aircraft; Aircraft propulsion; Cooling; Equations; Generators; Heating; Shafts;
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.1953.6371313
Filename
6371313
Link To Document