Aeroacoustic Analysis of a Counter Rotating Open Rotor based on the Harmonic Balance Method
Conference contribution, 2018

The Counter Rotating Open Rotor (CROR) powerplant is an interesting architecture for future regional aircraft propulsion since it offers higher propulsive efficiency and thereby lower fuel consumption than the conventional Turbofan engine. The noise levels generated are however potentially larger compared to a Turbofan due in part to the absence of a ducting nacelle. This raises the need for efficient, high fidelity tools that can be used for the design and evaluation of new blade concepts capable of meeting strict noise regulations. In this paper, a Computational Aeroacoustics (CAA) platform for CRORs based on the Harmonic Balance method is presented. The method is formulated in the time domain and solves for the dominant frequencies of the flow by expressing the solution as a truncated Fourier series in time. Coupling between the resolved frequencies is furthermore possible since the nonlinear URANS equations are solved for. The far field acoustic signature is obtained by solving a convective form of the Ffowcs Williams-Hawkings equations for permeable surfaces. The CAA platform is applied to a generic, full scale, pusher type CROR operating at cruise conditions.

Open

Counter

Computational

Rotating

Balance

Rotor

Aeroacoustics

Propeller

Ffowcs-Williams Hawkings

Harmonic

Author

Daniel Lindblad

Chalmers, Mechanics and Maritime Sciences, Fluid Dynamics

Gonzalo Montero Villar

Chalmers, Mechanics and Maritime Sciences, Fluid Dynamics

Niklas Andersson

Chalmers, Mechanics and Maritime Sciences, Fluid Dynamics

Alexandre Capitao Patrao

Chalmers, Mechanics and Maritime Sciences, Fluid Dynamics

Suk-kee Courty-Audren

University of Toulouse

Gaël Napias

University of Toulouse

Areas of Advance

Transport

Subject Categories

Aerospace Engineering

Fluid Mechanics and Acoustics

Infrastructure

C3SE (Chalmers Centre for Computational Science and Engineering)

DOI

10.2514/6.2018-1004

More information

Latest update

2/21/2018