Title :
Air-turbine drives: Performance and limitations
Author_Institution :
Stratos, Division of Fairchild Engine and Airplane Corporation, Bay Shore, N. Y.
fDate :
4/1/1956 12:00:00 AM
Abstract :
This article discusses the imposed requirements at the design point, or when receiving a minimum of high-pressure air supply from the compressor, and the penalty involved at the cruise condition. Turbine configurations and control-system response rates are compared.
Keywords :
Airplanes; Ducts; Electrical engineering; Engines; Temperature dependence; Turbines;
Journal_Title :
Electrical Engineering
DOI :
10.1109/EE.1956.6441837
