Comparisons of rig and engine dynamic events in the compressor of an axi-centrifugal turboshaft engine /

Bibliographic Details
Main Authors:	Owen, A. Karl (Author), Mattern, Duane L. (Duane Loren) (Author), Le, Dzu K. (Author)
Corporate Authors:	U.S. Army Research Laboratory (sponsoring body.), United States. National Aeronautics and Space Administration (sponsoring body.)
Format:	Government Document eBook
Language:	English
Published:	Cleveland, Ohio : National Aeronautics and Space Administration, Lewis Research Center : U.S. Army Research Laboratory, October 1996.
Series:	NASA technical memorandum ; 107339. ARL-TR (Aberdeen Proving Ground, Md.) ; 1108.
Subjects:	Gas turbine engines. Compressors. Fourier analysis. Surges. Rotating stalls. Modal response. Traveling waves. Aircraft engines.
Online Access:	https://purl.fdlp.gov/GPO/gpo70389

Description
Item Description:	Title from title screen (viewed July 26, 2016). "October 1996"--Report documentation page. "Prepared for the 41st Gas Turbine and Aeroengine Congress sponsored by the International Gas Turbine Institute of the American Society of Mechanical Engineers, Birmingham, United Kingdom, June 10-13, 1996." "Performing organization: NASA Lewis Research Center and Vehicle Propulsion Directorate, U.S. Army Research Laboratory"--Report documentation page. "ASME 96-GT-239."
Physical Description:	1 online resource (9 pages) : illustrations.
Bibliography:	Includes bibliographical references (page 9).