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Acoustics Considerations for Propulsion Airframe IntegrationMany NASA and industry advanced airframe configurations involve highly integrated installations of the propulsion system either directly into the airframe or in close proximity. Current acoustic challenges resulting from highly integrated propulsion installations will be reviewed as well as the ongoing NASA efforts to quantify these impacts to improve noise estimates of future systems and guide noise reduction technology maturation activities.
Document ID
20190032075
Acquisition Source
Glenn Research Center
Document Type
Conference Paper
Authors
Van Zante, Dale
(NASA Glenn Research Center Cleveland, OH, United States)
Elliott, David M.
(NASA Glenn Research Center Cleveland, OH, United States)
Date Acquired
October 15, 2019
Publication Date
September 22, 2019
Subject Category
Spacecraft Propulsion And Power
Report/Patent Number
GRC-E-DAA-TN71888
Report Number: GRC-E-DAA-TN71888
Meeting Information
Meeting: ISABE 2019 (International Society for Air Breathing Engines)
Location: Canberra
Country: Australia
Start Date: September 22, 2019
End Date: September 27, 2019
Sponsors: International Society for Air Breathing Engines (ISABE)
Funding Number(s)
WBS: 081876.02.03.50.03.06
Distribution Limits
Public
Copyright
Portions of document may include copyright protected material.
Technical Review
Single Expert
Keywords
Propulsion Airframe Integration
Propulsion Airframe Aeroacoustics
Acoustic liners
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