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Progress Toward Improving Jet Noise Predictions in Hot JetsAn acoustic analogy methodology for improving noise predictions in hot round jets is presented. Past approaches have often neglected the impact of temperature fluctuations on the predicted sound spectral density, which could be significant for heated jets, and this has yielded noticeable acoustic under-predictions in such cases. The governing acoustic equations adopted here are a set of linearized, inhomogeneous Euler equations. These equations are combined into a single third order linear wave operator when the base flow is considered as a locally parallel mean flow. The remaining second-order fluctuations are regarded as the equivalent sources of sound and are modeled. It is shown that the hot jet effect may be introduced primarily through a fluctuating velocity/enthalpy term. Modeling this additional source requires specialized inputs from a RANS-based flowfield simulation. The information is supplied using an extension to a baseline two equation turbulence model that predicts total enthalpy variance in addition to the standard parameters. Preliminary application of this model to a series of unheated and heated subsonic jets shows significant improvement in the acoustic predictions at the 90 degree observer angle.
Document ID
20070012405
Acquisition Source
Glenn Research Center
Document Type
Contractor Report (CR)
Authors
Khavaran, Abbas
(ASRC Aerospace Corp. Cleveland, OH, United States)
Kenzakowski, Donald C.
(Combustion Research and Flow Technology, Inc. Pipersville, PA, United States)
Date Acquired
August 23, 2013
Publication Date
February 1, 2007
Subject Category
Acoustics
Report/Patent Number
AIAA Paper 2007-0012
NASA/CR-2007-214671
E-15807
Report Number: AIAA Paper 2007-0012
Report Number: NASA/CR-2007-214671
Report Number: E-15807
Meeting Information
Meeting: 45th Aerospace Sciences Meeting and Exhibit
Location: Reno, NV
Country: United States
Start Date: January 8, 2007
End Date: January 11, 2007
Funding Number(s)
CONTRACT_GRANT: NNC06BA07B
WBS: WBS 561581,92,98.03.18.03
Distribution Limits
Public
Copyright
Public Use Permitted.
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