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From
Experimental Assessment of Noise Generation from I.C. Engine Intake and Exhaust Systems Components
Sabry Allam
American Journal of Vehicle Design
.
2015
, 3(1), 6-15
Figure
1.
Measurement configuration for plane wave decomposition at MWL.(a) Constructor drawing of the test rig that is used with Case 1 (single orifice) and Case 2 (double orifices), (b) Photo for the test rig with SR is connected
Full size figure and legend
Figure
2.
The test objects, (a) a single diaphragm orifice with a concentric hole with t/d
o
=0.17 and do/d
i
=0.63, (b) double orificest/d
o
=0.17, di/d
o
=0.63, L=3d
o
(c)ovalshape resonator, (d) complex side branch resonator(e)two side-branches in series (compact resonator)
Full size figure and legend
Figur
e 3.
Amplification of sound for the tested orifice at (a) M=0.0482, (b) M= 0.0675
Full size figure and legend
Figure
4.
Plot of D(ω) in the complex plane for a system consisting of the tested orifice and free terminationup and downstream duct at M=0.0675
Full size figure and legend
Figure
5.
Amplification of sound for the tested double orifices at(a) M=0.02, (b) M=0.033, (c) M= 0.05.L=3D
o
Full size figure and legend
Figure
6.
Plot of D(ω) in the complex plane for a system consisting of the tested double orifices and free terminationup and downstream duct
Full size figure and legend
Figure
7.
Source term according calculated according to Eq.(3) for double orificesat three different speeds
Full size figure and legend
Figure
8
.
Amplification of sound for the resonator shown in Figure 2(c) at different Mach numbers.(a)M=0.05, (b) M=0.10, d
in
=0.066m
Full size figure and legend
Figure
9.
Amplification of sound for the resonator shown in Figure 2(d) at different Mach numbers. (a)M=0.05, (b) M=0.1, d
in
=.034m
Full size figure and legend
Figure
10.
Plot of D(ω) in the complex plane for a system consisting of the tested side branch resonator and free termination up and downstream duct
Full size figure and legend
Figure
11.
Amplification of sound for the resonator shown in Figure 2(e) at different Mach number.(a) M=0.025, (b) M=.05, (c) M=0.1, d
o
=0.037 m
Full size figure and legend
Figure
12.
Amplification of sound for the tested double orifices at(a) M=0.025, (b) M=0.05, (c) M= 0.1
Full size figure and legend
Figure
13.
Source term according calculated according to Eq.(3) compact side branch resonator at three different speeds
Full size figure and legend