Aeroacoustic performance of multi-stream, rectangular, supersonic jets

Scott M. Hromisin, Junichi Akatsuka, Dennis K. McLaughlin, Philip John Morris

Research output: Chapter in Book/Report/Conference proceedingConference contribution

Abstract

Multi-stream, variable cycle point, turbofan engines with rectangular exhaust profiles are in consideration for future tactical aircraft. Such engine architectures aim to combine the benefits of low-profile, simple geometry nozzles with the ability to cycle between high-thrust and high-efficiency operation as required by the demands of the flight profile. There exists a need to improve the understanding of the aeroacoustic characteristics of low bypass ratio, multi-stream rectangular exhaust jets. This work reports on a series of experiments that have been performed in an effort to begin meeting this demand. Model-scale far field acoustic data are reported for heat-simulated, supersonic, dual stream, rectangular jets. Acoustic data are compared with far field noise measurements of single round and rectangular jets operating at equivalent thrust and mass flow rate jet conditions. Dual stream jets demonstrate the potential for noise reductions over 4 dB OASPL in the peak noise emission direction compared to single stream equivalent jets.

Original languageEnglish (US)
Title of host publicationAIAA Scitech 2019 Forum
PublisherAmerican Institute of Aeronautics and Astronautics Inc, AIAA
ISBN (Print)9781624105784
StatePublished - Jan 1 2019
EventAIAA Scitech Forum, 2019 - San Diego, United States
Duration: Jan 7 2019Jan 11 2019

Publication series

NameAIAA Scitech 2019 Forum

Conference

ConferenceAIAA Scitech Forum, 2019
CountryUnited States
CitySan Diego
Period1/7/191/11/19

Fingerprint

Aeroacoustics
Bypass ratio
Turbofan engines
Acoustic fields
Noise abatement
Acoustic noise
Nozzles
Acoustics
Aircraft
Flow rate
Engines
Geometry

All Science Journal Classification (ASJC) codes

  • Aerospace Engineering

Cite this

Hromisin, S. M., Akatsuka, J., McLaughlin, D. K., & Morris, P. J. (2019). Aeroacoustic performance of multi-stream, rectangular, supersonic jets. In AIAA Scitech 2019 Forum (AIAA Scitech 2019 Forum). American Institute of Aeronautics and Astronautics Inc, AIAA.
Hromisin, Scott M. ; Akatsuka, Junichi ; McLaughlin, Dennis K. ; Morris, Philip John. / Aeroacoustic performance of multi-stream, rectangular, supersonic jets. AIAA Scitech 2019 Forum. American Institute of Aeronautics and Astronautics Inc, AIAA, 2019. (AIAA Scitech 2019 Forum).
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abstract = "Multi-stream, variable cycle point, turbofan engines with rectangular exhaust profiles are in consideration for future tactical aircraft. Such engine architectures aim to combine the benefits of low-profile, simple geometry nozzles with the ability to cycle between high-thrust and high-efficiency operation as required by the demands of the flight profile. There exists a need to improve the understanding of the aeroacoustic characteristics of low bypass ratio, multi-stream rectangular exhaust jets. This work reports on a series of experiments that have been performed in an effort to begin meeting this demand. Model-scale far field acoustic data are reported for heat-simulated, supersonic, dual stream, rectangular jets. Acoustic data are compared with far field noise measurements of single round and rectangular jets operating at equivalent thrust and mass flow rate jet conditions. Dual stream jets demonstrate the potential for noise reductions over 4 dB OASPL in the peak noise emission direction compared to single stream equivalent jets.",
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Hromisin, SM, Akatsuka, J, McLaughlin, DK & Morris, PJ 2019, Aeroacoustic performance of multi-stream, rectangular, supersonic jets. in AIAA Scitech 2019 Forum. AIAA Scitech 2019 Forum, American Institute of Aeronautics and Astronautics Inc, AIAA, AIAA Scitech Forum, 2019, San Diego, United States, 1/7/19.

Aeroacoustic performance of multi-stream, rectangular, supersonic jets. / Hromisin, Scott M.; Akatsuka, Junichi; McLaughlin, Dennis K.; Morris, Philip John.

AIAA Scitech 2019 Forum. American Institute of Aeronautics and Astronautics Inc, AIAA, 2019. (AIAA Scitech 2019 Forum).

Research output: Chapter in Book/Report/Conference proceedingConference contribution

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Hromisin SM, Akatsuka J, McLaughlin DK, Morris PJ. Aeroacoustic performance of multi-stream, rectangular, supersonic jets. In AIAA Scitech 2019 Forum. American Institute of Aeronautics and Astronautics Inc, AIAA. 2019. (AIAA Scitech 2019 Forum).