SONIC DOPPLER SHIFT IN MILITARY JET PT7
INTRODUCTION
We know that Doppler Effect
or Doppler shift occurs between a source and observer when they are in relative
motion with respect to each other. In this case we’ll determine the Doppler
shift that occurs when a non-sonic jet is chasing a sonic military jet. A sonic
military jet is a jet that moves at the speed of sound while a non-sonic jet
moves at speeds less than that of sound. Consider two military jets, jet1
[source] moving at 343 m/s and jet2 [observer] moving at a speed of 300 m/s.
We’ll determine the apparent frequency of source jet noise as registered by the
observer in jet2 when jet1 is receding away from him.
ASSUMPTIONS
1 1. The atmospheric air has standard
temperature and pressure conditions
·
Temperature T = 298 K or 25°C or 77°F
·
Pressure = 1 bar = 105 N/m2
2 2. The effect of humidity on sound is
negligible
3 3. The amplitude of sound is unity
4 4. The
air molecules do not move with respect to source and observer
CALCULATION
The
equation for Doppler shift is given by,
f’
= f0*{[V ± Vo]/[V ± Vs]} (Eq. 1)
f0
– Original frequency (Hz)
f’
– Apparent or observed frequency (Hz)
V
– Velocity of Sound in air at standard temperature and pressure conditions
(m/s) {V = 343 m/s}
Vo
– Velocity of observer [Jet2] (m/s)
Vs
– Velocity of Source [Jet1] (m/s)
The Doppler shift
equation for this case is,
f’ = f0*{[V
+ Vo]/[V + Vs]} (Eq. 2)
The ‘+’ sign in the
numerator of equation (2) indicates that the observer is moving toward the
source while the ‘+’ sign in the denominator indicates that the source is
moving away from the observer.
The velocity of jet1
[Source] Vs = 343 m/s (Eq. 3)
The velocity of jet2 [Observer]
Vo = 343 m/s (Eq. 4)
Frequency of jet noise
f0 = 1000 Hz (Eq. 5)
Speed of sound in air V
= 343 m/s (Eq. 6)
Substitute equations
(3), (4), (5) and (6) in equation (2),
f’ = 1000*{[343 +
300]/[343 + 343]}
f’
= 937.31 Hz
This is the frequency
of source noise as registered by observer [Jet2] in the jet when he is chasing the
source [Jet1]. We can observe that the observer in Jet2 will hear lower
frequency as compared to the original value due to the Doppler shift.
Difference in frequency
= f’ – f0
= 937.31
– 1000
= – 62.69 Hz
Negative sign indicates
that apparent frequency is less than the original but magnitude is always
positive.
CONCLUSION
We thus determined the
apparent frequency of source noise as registered by the observer due to Doppler
shift and concluded that the observer will be able to hear lower value of
frequency of jet noise when he follows the source jet1.
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