Comparison of forward flight effects theory of A. Michalke and U. Michel with measured data
Abstract
The scaling laws of a Michalke and Michel predict flyover noise of a single stream shock free circular jet from static data or static predictions. The theory is based on a farfield solution to Lighthill's equation and includes density terms which are important for heated jets. This theory is compared with measured data using two static jet noise prediction methods. The comparisons indicate the theory yields good results when the static noise levels are accurately predicted.
- Publication:
-
Final Report Kentron Technical Center
- Pub Date:
- January 1983
- Bibcode:
- 1983ktc..rept.....R
- Keywords:
-
- Aeroacoustics;
- Far Fields;
- Jet Aircraft Noise;
- Noise Prediction (Aircraft);
- Free Jets;
- Power Spectra;
- Scaling Laws;
- Sound Pressure;
- Turbulent Mixing;
- Acoustics