Determination of Installed Versus Dynamometer Horsepower for Utility-Type Aircraft
Published January 1, 1964 by SAE International in United States
Annotation of this paper is available
The problems of developing power charts which accurately reflect the installed engine performance in utility-type aircraft, and the use of recently developed in-flight torquemeters as an aid in this development are discussed. Techniques in use of the torquemeter for the development of various installation components is also presented.