NASA Logo

NTRS

NTRS - NASA Technical Reports Server

Back to Results
Acoustic design of the QCSEE propulsion systemsAcoustic design features and techniques employed in the Quiet Clean Short-Haul Experimental Engine (QCSEE) Program are described. The role of jet/flap noise in selecting the engine fan pressure ratio for powered lift propulsion systems is discussed. The QCSEE acoustic design features include a hybrid inlet (near-sonic throat velocity with acoustic treatment); low fan and core pressure ratios; low fan tip speeds; gear-driven fans; high and low frequency stacked core noise treatment; multiple-thickness treatment; bulk absorber treatment; and treatment on the stator vanes. The QCSEE designs represent and anticipated acoustic technology improvement of 12 to 16 PNdb relative to the noise levels of the low-noise engines used on current wide-body commercial jet transport aircraft.
Document ID
19780016124
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Loeffler, I. J.
(NASA Lewis Research Center Cleveland, OH, United States)
Smith, E. B.
(GE Co. Fairfield, Conn., United States)
Sowers, H. D.
(GE Co. Fairfield, Conn., United States)
Date Acquired
August 9, 2013
Publication Date
January 1, 1976
Publication Information
Publication: NASA. Langley Res. Center Powered-Lift Aerodyn. and Acoustics
Subject Category
Aerodynamics
Accession Number
78N24067
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
No Preview Available