Pusher propeller noise directivity and trends
Abstract
The effects of pylon wake interaction on far-field propeller noise are studied using a model scale SR-2 propeller in a low-speed anechoic wind tunnel. The variation in the pusher noise penalty with axial angle theta and circumferential angle phi is compared to that of the tractor noise penalty; and the former exhibits minima occurring in the propeller plane and maxima occurring toward the propeller axis. The magnitude of the pusher installation noise penalty decreased with in increase in shaft horsepower and tip Mach number. Directivity comparisons revealed that both a noise reduction and a directivity pattern change resulted when the pylon was moved farther from the propeller. Noise emerging from the wake interaction was distinguished from that of the propeller by means of a modal decomposition.
- Publication:
-
Thermophysical Aspects of Re-entry Flows
- Pub Date:
- July 1986
- Bibcode:
- 1986aiaa.confU....B
- Keywords:
-
- Aerodynamic Noise;
- Directivity;
- Noise Intensity;
- Noise Reduction;
- Propellers;
- Wind Tunnel Tests;
- Modal Response;
- Nacelles;
- Pushing;
- Pylons;
- Struts;
- Subsonic Wind Tunnels;
- Turbofan Aircraft;
- Acoustics