Comparative Study of Impedance Eduction Methods: DLR Tests and Methodology - Part 1The absorption efficiency of acoustic liners used in aircraft engines is characterized by the acoustic impedance. World wide, many grazing ow test rigs and eduction methods are available that provide values for that impedance. However, a direct comparison and assessment of the data of the di erent rigs and methods is often not possible because test objects and test conditions are quite di erent. Only a few papers provide a direct comparison. Therefore, this paper together with a companion paper, present data measured with a reference test object under similar conditions in the DLR and NASA grazing ow test rigs. Additionally, by applying the in-house methods Liner Impedance Non-Uniform ow Solving algorithm (LINUS, DLR) and Convected Helmhholtz Equation approach (CHE, NASA) on the data sets, similarities and differences due to underlying theory are identi ed and discussed.
Document ID
20130013987
Acquisition Source
Langley Research Center
Document Type
Conference Paper
Authors
Busse-Gerstengarbe, Stefan (Technische Univ. Berlin, Germany)
Bake, Friedrich (German Aerospace Center Berlin)
Enghardt, Lars (Technische Univ. Berlin, Germany)
Jones, Michael G. (NASA Langley Research Center Hampton, VA, United States)
Date Acquired
August 27, 2013
Publication Date
May 27, 2013
Subject Category
Acoustics
Report/Patent Number
NF1676L-15559Report Number: NF1676L-15559
Meeting Information
Meeting: 19th AIAA/CEAS Aeroacoustics Conference
Location: Berlin
Country: Germany
Start Date: May 27, 2013
End Date: May 29, 2013
Sponsors: American Inst. of Aeronautics and Astronautics