TY - GEN
T1 - A Parametric Investigation of Rotor-Rotor Interaction Noise Generation
AU - Rau, Robert F.
AU - Greenwood, Eric
N1 - Funding Information:
The development of OpenCOPTER was supported by the NASA Revolutionary Vertical Lift Technology project through a cooperative agreement with the National Institute of Aerospace (80LARC17C004 Sub-Award C20-202030-PSU) with technical monitor Dr. Kyle A. Pascioni of the NASA Langley Research Center. This research was also partially supported by Blue Ridge Research and Consulting under NASA Phase I STTR 22-1-T15.04-1263 with technical monitor Samuel R. Kantor of the NASA Armstrong Flight Research Center.
Publisher Copyright:
Copyright © 2023 by the Vertical Flight Society. All rights reserved.
PY - 2023
Y1 - 2023
N2 - An extensive parametric study of a two rotor system configurations is conducted to investigate the effect of rotor placement on noise generation, with the aim of providing preliminary design information to multirotor aircraft designers. A computationally efficient wake method called OpenCOPTER is used to conduct the aerodynamic simulations and PSU-WOPWOP is used to predict the rotor sound power level over an acoustic hemisphere. An extensive parameter sweep is explored consisting of several different rotor placements and operating conditions. Aerodynamic interactions between the rotors are found to result in significant rotor-rotor interaction noise when the downstream rotor is placed in two different regions behind the upstream rotor. The rotor-rotor interaction noise also varies as the rotors are offset laterally. Even for conditions where rotor-rotor interaction noise does not occur, aerodynamic interactions between the rotors can affect how rotors interact with their own wake. Positioning the downstream rotor above, but relatively close to, the upstream rotor is shown to result in a robust reduction in noise across the entire operating envelope.
AB - An extensive parametric study of a two rotor system configurations is conducted to investigate the effect of rotor placement on noise generation, with the aim of providing preliminary design information to multirotor aircraft designers. A computationally efficient wake method called OpenCOPTER is used to conduct the aerodynamic simulations and PSU-WOPWOP is used to predict the rotor sound power level over an acoustic hemisphere. An extensive parameter sweep is explored consisting of several different rotor placements and operating conditions. Aerodynamic interactions between the rotors are found to result in significant rotor-rotor interaction noise when the downstream rotor is placed in two different regions behind the upstream rotor. The rotor-rotor interaction noise also varies as the rotors are offset laterally. Even for conditions where rotor-rotor interaction noise does not occur, aerodynamic interactions between the rotors can affect how rotors interact with their own wake. Positioning the downstream rotor above, but relatively close to, the upstream rotor is shown to result in a robust reduction in noise across the entire operating envelope.
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M3 - Conference contribution
AN - SCOPUS:85167696284
T3 - FORUM 2023 - Vertical Flight Society 79th Annual Forum and Technology Display
BT - FORUM 2023 - Vertical Flight Society 79th Annual Forum and Technology Display
PB - Vertical Flight Society
T2 - 79th Vertical Flight Society Annual Forum and Technology Display, FORUM 2023
Y2 - 16 May 2023 through 18 May 2023
ER -