Abstract
The current emphasis on environment protection by reducing noise pollution has led to stricter noise standards for general aviation aircraft. As a result, there is a growing demand for a computational tool to predict the noise during the design process. A computer program, called ProRAPP, has been developed for the prediction of noise generated by propeller/rotor blades. The acoustic pressure is calculated using a form of Ffowcs Williams-Hawkings equation which is suitable for numerical implementation. For noise predictions, the observer can either move with the propeller/rotor hub or it can be fixed to the ground. Experimental data from both wind tunnel and flight tests are used to validate the numerical results.
Original language | English |
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Journal | SAE Technical Papers |
DOIs | |
State | Published - 1998 |
Event | 1998 World Aviation Conference - Anaheim, CA, United States Duration: Sep 28 1998 → Sep 30 1998 |