Getting to Grips with Aircraft Noise
Getting to Grips with Aircraft Noise
Getting to Grips with Aircraft Noise
Create successful ePaper yourself
Turn your PDF publications into a flip-book with our unique Google optimized e-Paper software.
2.1.2. FAN NOISE<br />
Flight Operations Support & Line Assistance<br />
<strong>Getting</strong> <strong>to</strong> grips <strong>with</strong> aircraft noise<br />
2 - AIRPLANE NOISE SOURCES<br />
The noise produced by the fan results of the superimposition of a wide-band noise (as<br />
for the jet) and noise <strong>with</strong> harmonics.<br />
• The wide band noise is due <strong>to</strong> the boundary layer developing on the fan blades,<br />
and more generally <strong>to</strong> the airflow around them.<br />
• The harmonics are originating in the intrinsic cycling character of the fan motion<br />
(spinning motion). The most remarkable frequency is the fundamental, the value<br />
of which is the number of blades times the fan rotation speed. The harmonics are<br />
multiples of this fundamental.<br />
• When the engine rating is high (during takeoff for instance), the airflow around<br />
the fan blades transitions <strong>to</strong> supersonic and these multiple pure <strong>to</strong>nes are at the<br />
origin of a the so-called “buzz saw noise”.<br />
2.1.3. COMPRESSOR NOISE<br />
It is of the same kind than the fan noise, but the harmonics are less emergent due <strong>to</strong><br />
interaction phenomena.<br />
2.2. AIRFRAME NOISE<br />
The airframe noise would be the noise produced by the aircraft, if all engines were<br />
made inoperative. It is generated by the airflow surrounding the moving plane. The main<br />
sources are the discontinuities of the aircraft structure, such as high-lift devices, landing<br />
gear wheels (when extended), trailing edges where there is a speed shearing (aircraft<br />
speed versus still air).<br />
It was empirically determined that the noise emissions are dependent on the sixth<br />
power of the aircraft’s true airspeed. This noise produced from aerodynamic<br />
phenomena is most sensitive during approach, when engine power is the lowest.<br />
2.3. EXAMPLE OF SHARE BETWEEN ENGINE AND<br />
AERODYNAMIC NOISE<br />
The following sketches illustrate the share between engine parts and airframe regarding<br />
noise emissions.<br />
7