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ME 322: Instrumentation Lecture 32. April 11, 2014 Professor Miles Greiner. Announcements/Reminders. Next week: Lab 10 Vibrating Beam Extra-Credit LabVIEW Workshop Friday , April 18, 2014, 2-4 PM, Jot Travis Room 125D Sign-up on WebCampus - PowerPoint PPT Presentation
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ME 322: InstrumentationLecture 32
April 10, 2015Professor Miles Greiner
Announcements/Reminders• HW 10 due Monday
• I’m having trouble getting the date for the sample lab so I will post the new lab instructions (including L10PP), the sample data, and the sample report by the end of today… (sorry for taking so long)
• Marissa Tsugawa will hold a problem review session on Sunday– Will email time and place
• Next week: Lab 10 Vibrating Beam• Did you know?
– HW solutions are posted on WebCampus– Exam solution posted outside PE 213 (my office)
• Help wanted (see me [email protected]) – Spring 2016: ME 322 Lab Assistant
Cylinder in Cross Flow (unsteady)
• Speed is reduced in the wake region • Instability of steady flow causes periodically-shed vortices
– Karman Vortex Street• Figure shows unsteady speed measured by a probe in wake
– Fairly regular oscillations, period P ~ 0.01/6 = 0.0017 sec– Peak oscillatory frequency of f = 1/P ~ 600 Hz
• Broad spectrum of frequencies – Can a Pitot probe measure oscillations at these high frequencies?
• How to measure rapidly changing speeds?
V∞ VelocityProbe
Strouhal Number
• What does the vortex shedding frequency depend on?– Increases with – Decreases with
• Dimensionless Strouhal Number– ;
• For , 0.20 < < 0.21 (~constant)– Frequency increases linearly with speed and flow rate– This phenomena used to measure pipe volume flow rate Q
V∞
D Qf
Q
Example
• A car in Reno is moving at 60 miles/hour and has a ¼-inch diameter antenna. At what frequency will vortices be shed from it? The air temperature is 27°C and the atmospheric pressure is 86 kPa.
• 0.20 < < 0.21– For
How to measure Rapidly Varying Speed?
• Pressure Method– Pitot probes transmit pressure to transducers using tubes– This is ok for slowly varying speeds– At high frequencies, pressure response at transducer is attenuated and delayed compared to probe (2nd order
system)• Heat Transfer Method
– Hot Wire or Hot Film probe• Very small wire or metal plated quartz on a support fork
– Electrically heated surface– Heat transfer to the surrounding fluid increases with fluid speed– Two modes:
• Constant Current (film get cooler when speed increases)• Constant Temperature (more power is required to maintain temperature at high speed)
Hot wire/film circuit Circuit
• Probe electrical resistance heating– Q = IVO (can be measured)
• Heat is mostly removed by convection – Q = IVO= hA(TS-T∞)
• Neglecting radiation and conduction
• Convection Coefficient for small cylinders in cross flow– ; M and N are constants
• If we can find sensor temperature TS, then we can find – and
𝑉 ∞
hVO
V∞ T∞
I
VE
I
TS RS
R2
How to find TS?• Wire resistance depends on TS
• Temperature Coefficient of Resistance (material property)• RS0 = RS at T = T0
– , – We can find – So, theoretically we can find TS and so
• and
• Two modes of operation
Constant Current Mode
• Excitation voltage VE = constant, and R2 >> RS • = constant• Probe temperature TS and resistance RS go downs as V∞ goes up• Measure V0 = IRS
– V0 will decrease as V∞ increases– Calibrate
• Problem: Sensor temperature TS must reach equilibrium with its surroundings– Takes time, ~ 0.01 sec, or frequency 100 Hz
• Too slow!
VO
V∞ T∞
I
VE
I
TS RS
R2
V0
V∞
Constant Temperature Anemometer (CTA)
• Incorporates hot sensor into a Wheatstone bridge• If speed V∞ increases, TS and RS “start” to go down• This decreases VBridge, but Feedback amplifier (op-amp) very quickly
increases VO to increase current to sensor and restore its temperature and resistance (RS = RR)
• The current and power to the sensor adjusts to make its temperature constant• Output is VCTA (voltage across sensor)
V∞
VBridge
VCTA
TS RS
RR
CTA Transfer Function• Convection Heat Transfer from probe to fluid• )
• So – )– )– Or find constants a and b by calibration
• Feedback amplifiers respond very quickly– Accurate for up to f = 400,000 Hz– Requires feedback control (Lab 12)
• To use CTA, measure VCTA.– Calculate ,
Constants
Hot Film System Calibration
• The fit equation VCTA2 = aSA
0.5+b appears to be appropriate for these data.
• The dimensional parameters are – a = 1.366 volts2s1/2/m1/2 and – b = 2.2057 volts2
Lab 11 Unsteady Speed in a Karman
Vortex Street
• Use the same wind tunnels as Lab 6– Sign up for 1.5 hour periods with your partner in lab next week
• Two steps– Statically calibrate hot film CTA using a Pitot probe– Measure unsteady speed downstream from a cylinder of diameter D
• Perform spectral analysis and find frequency with peak amplitude, fP • Measure “steady” speed without cylinder V• Calculate StD = DfP /V and compare to expectations
Setup
• Add CTA and cylinder in cross flow • Do not use Venturi tube or Gage
Pressure Transducer– Assume Pstat = PATM (Pgage = 0)
• Tunnel Air Density
DTube
PP
Static
Total+ -
IP
Variable SpeedBlower Plexiglas
Tube
Pitot-Static Probe VC
3 in WC
BarometerPATM TATM
CTA
myDAQ
Cylinder
VCTA
Before Experiment• Construct VI (formula block)• Measure PATM, TATM, and cylinder D • Find m and r for air
• Air Viscosity from A.J. Wheeler and A. R. Ganji, Introduction to Engineering Experimentation, 2nd Edition, Pearson Prentice Hall, 2004, p. 430.
T D P m r
Kelvin inch kPa N-s/m2 Kg/m3296.2 0.125 88.1 1.8262E-05 1.037
Fig. 2 VI Block Diagram
Spectral Measurements Selected Measurements: Magnitude (RMS) View Phase: Wrapped and in Radians Windowing: Hanning Averaging: None
Formula Formula: ((v**2-b)/a)**2
Fig. 1 VI Front Panel
Calibrate CTA using Pitot Probe
• Remove Cylinder• Align hot film and Pitot probes (carefully)
– 4 probes cost $600• Measure VCTA,AVG and IPitot for different blower
speeds
Calibration Measurements and Calculations
• Average Velocity•
IP VCTA PP VA VA1/2 VCTA
2 di2=(aVA
1/2+b-VCTA2)2
[mA] [V] [Pa] [m/s] [m/s]1/2 [V2] [V4]
Table 2 Calibration Data
• The initial and final no-wind hot film voltages and Pitot transmitter currents are the same.
IP
[mA]VCTA
[V]SA
[m/s]SA
1/2
[m1/2/s1/2]VCTA
2
[V2]4.00 2.140 0 0.00 4.585.70 3.670 12 3.52 13.477.40 3.930 17 4.18 15.449.40 4.070 22 4.70 16.5611.60 4.130 26 5.11 17.0616.80 4.460 34 5.83 19.8914.40 4.340 31 5.53 18.8413.30 4.290 29 5.38 18.4011.00 4.160 25 5.01 17.318.50 4.000 20 4.49 16.006.30 3.820 14 3.79 14.594.00 2.140 0 0.00 4.58
Standard Error of the Estimate
• Find best fit line
• Find Standard Error of the Estimate
• Now measure VCTA to determine
xxxx
x
x
xx
VCTA2 𝑆√𝑉 𝐴
𝑆𝑉𝐶𝑇𝐴2
√𝑉 𝐴
Measure VCTA to determine
• Invert
• Uncertainty
• But we want
Cylinder in cross flow
Wake: region of reduced speed
Frequency
Strughold #:
For
Constant
Page 360 to 361
Measure flow rate in a pipe
Example
A car antenna D = 0.25 in and car s=60 mphWhat will the frequency of the shed vortices be?
Before we used: Pressure Method
Pito-probe/pressure transmitter (too slow)
Heat transfer method:
-hot film or hot wire probe
-small electrically heated surface
Probe:
Acid etched wire (hot wire)
-small but brittle
Metal plated quartz cylinder (hot film).
Probe electrical resistance heating
→ Can measure I, V0 Q [watts]
Heat is mostly dissipated by convection
For small cylinders in cross flow
How to find TS:
Wire resistance changes with its temperature TS:
α ≡ material property
So theoretically by measuring: A, I, V0, & known α.
Tow modes of operation:1) Constant current
VE ≡ constant & R2 >> RS
As U↑, h↑, TS↓, RS↓
Problem:
TS must reach equilibrium with surroundings.
Takes time
Max frequency Response
2) Constant Temp Anemometer (CTA)•Uses electronic feedback (op-amp) to very VE so TS (and RS) stay constant.
Wheat stone bridge circuit