Upload
others
View
18
Download
0
Embed Size (px)
Citation preview
NIST’s New 3D Airspeed Calibration Rig Addresses Turbulent Flow Measurement Challenges
Authors: Iosif Shinder, Vladimir Khromchenko, Michael Moldover
Is this research important?There are at least two reasons why it is important: 1. Humanitarian: Let’s keep the Earth a habitable place
for future generations! 2. Mercantile: A lot of money involved!
What is this talk about?
• Why we are doing 2-D and 3-D calibrations?• 3-D Calibration Rig.• How turbulence intensity affects calibration.• Traditional turbulence generators.• Flag-like turbulence generator.• How to measure turbulence?• Low turbulence s-probe calibration.• Pitot tube and s-probe in turbulent flows.
Flow is Complicated
Real stacks have swirls and turbulence
Flow is Complicated
Real stacks have skew
How are Emissions Measurements Made Today?Emission is a product of concentration and flow
Flow Problems:
No Traceability to NIST
There is so called: Annual “Relative Accuracy Test Audit” (RATA) which “calibrates” continuous emission flow monitors (usually ultrasonic flowmeter). Typically, the flow is surveyed with S-probe and 5-hole pitot static probes, which are temporarily installed on the stack.
For S-probes the calibration factor is fixed and these probes can be used without calibration for certain specified geometries.
As the name suggests, the EPA protocols provide only relative accuracy, not uncertainty relative to primary standards. 6
Wind Tunnel Parameters
• Test volume: 2 m long × 1.5 m wide × 1.2 m high
• Airspeeds up to 75 m/s (165 mi/hour)
• Uncertainties – 0.42% increasing to 1% near 1 m/s
• Low (0.1 %) turbulence intensity; to increase turbulence, we install turbulence generators upstream of the test volume
VTuVσ
=
Y X
Z
Yaw Angle (around Y)
Pitch Angle (around Z, arc approximated using X and Y stages)
Automated 3D Pitot Tube Calibration Rig (2013)
2D S-Probe
3D Conic Probe
S-probe: workhorse for stack flow measurements
CheapStable
RuggedPassive
Can be calibrated
S-probe: cannot detect pitch
Flow Flow
≠Flow
≠
-30˚ pitch 0˚ pitch +30˚ pitch
S-Probe, (used in EPA protocol 2)
Calibration Factor is a Function of 4 variables1. Air speed2. Pitch angle3. Yaw angle4. Turbulence intensity
EPA protocol assumes calibration factor = 0.84(literature shows small, linear dependence on air speed)
11
EPA Method 2: S-Probe Calibration
Calibration data for one probe; others might be different.
-3
-2
-1
0
1
2
3
-180 -90 0 90 180
360˚ S-Probe response in 2˚ steps10 m/s; 0 °pitch
Yaw, [degree]
0 Yaw°
90 Yaw°
PP
∆
∆S-probe
Pitot
yaw angle, degrees-180 -90 0 90 180
-3
-2
-1
0
1
2
3
pitch angle 30 o
0 o
20 o
-10 o
-20 o
10 o
-30 o
NIST Calibration of S-Probe Flow: 10 m/s, turbulence intensity < 0.5%
Magnify 0 ° and 90 °PP
∆
∆S-probe
Pitot
--
-
yaw angle, degrees
-10 0 101.0
1.2
1.4
1.6
1.8
2.0
yaw angle, degrees
80 90 100
-0.4
-0.2
0.0
0.2
0.4 pitch angle
0 o
S-Probe (used for CEM per EPA protocol 2)flow: 10 m/s, turbulence intensity < 0.5%3 zeros ⇔
± 5 ° yaw uncertainty
± 5 ° yaw~8% cal
uncertainty
yaw angle, degrees
-10 0 101.0
1.2
1.4
1.6
1.8
2.0
yaw angle, degrees
80 90 100
-0.4
-0.2
0.0
0.2
0.4pitch angle
30 o
0 o
20 o
-10 o
-20 o
10 o
-30 o
S-Probe (used for CEM per EPA protocol 2)Flow: 10 m/s, turbulence intensity < 0.5%
Calibration depends upon pitch angle
---
Adapted from:“Experimental Study of the Factors Effect on the S type Pitot Tube Coefficient” Nguyen Doan Trang et. al. XX IMEKO World Congress
Effects of Pitch: Other Researchers
well-known for airfoils, unknown in Pitot tube literature
Calibration factor has hysteresis in low turbulenceIncreasing turbulence reduces hysteresis
18
Calibration of Multi-Hole Pitot Tubes
20o
RecirculationZone
Flow
19
Modify wind tunnel: addGrid to Generate Turbulence
Measure Effects of Grid. Periodic Structure.
FLOW
7.5
15
Large Scale Homogeneous Turbulence and Interactions with a Flat-Plate Cascade. Jon Vegard Larssen, Ph.D. Thesis.
Turbulence intensity probes
slope = 0.98
0
0.05
0.1
0.15
0.2
0 0.05 0.1 0.15 0.2
slope = 1.01
0
0.05
0.1
0.15
0.2
0 0.05 0.1 0.15 0.2
CobraTu
LDATu
LDATu
Hot wireTu −
0
0.05
0.1
0.15
0.2
0.25
0 0.02 0.04 0.06 0.08
25 m/s 20 m/s 15 m/s 10 m/s 5 m/s
2.5
3.5
4.5
5.5
0 10 20 30
( ) ( )1 2LDA
Pitot
Tu F V F TuTu
=
L-shape pitot tube turbulence calibration
0.98
1
1.02
1.04
0 0.05 0.1 0.15 0.2 0.25
Calib
ratio
n fa
ctor
LDA turbulence
10 m/s
( ) ( )1 2/ ReP NISTV V F F Tu=
( )2
21
2
P a TuVρ∆
= +
0
5
10
15
20
25
V, [m/s]
0.25
0.2
0.15
0.1
0.05
0 .99
0.99
0.995
0.995
1
1
1.005
1.005
1.01
1.01
1.015
1.015
1.02
1.02
1.025
1.025
1.03
1.03
Vpi
tot/V
NIS
T
Vpi
tot/V
NIS
T
-2.5
0
2.5
-180 -90 0 90 180
Yaw, [˚]
0˚ Pitch Angle0.27%5.20%8.60%13.80%
-2.5
0
2.5
-180 -90 0 90 180
Yaw, [˚]
-30˚ Pitch Angle
-2.5
0
2.5
-180 -90 0 90 180
Yaw, [˚]
+30˚ Pitch Angle
s probe
primary
PP
−∆
∆s probe
primary
PP
−∆
∆
s probe
primary
PP
−∆
∆
±3%0˚Flow direction
-30˚Flow direction
+30˚Flow direction
28
Summary1. NIST calibrates S-probes and 3D (multi-hole) probes.
2. S-probes can have multiple nulls. Incorrect nulling may cause errors during calibrations and measurements.
3. S-probes are sensitive to pitch angle; therefore, calibration factors does not represent measured flow.
4. Five-hole pitot tubes are sensitive to turbulence intensity.
5. Regular pitot tube and s-probe much less sensitive to turbulence.
6. NIST has studied only a few probes. How sensitive are other probes to turbulence?
We thank Greg Scace for design, assembly, and continuing support of the 3-D system
and
Jim Filla for writing 3-D system software and readiness to modify and improve it on first request.
The paper with the same title “NIST’s New 3D Airspeed Calibration Rig Addresses Turbulent Flow Measurement Challenges” was published in the proceedings of ISFFM, Arlington, Virginia, April 14-16, 2015