final report: specialist committee on uncertainty …...ittc 7.5-01-03-01 (2008) 16 instrument...
TRANSCRIPT
Specialist Committee on Uncertainty Analysis
Joel T. Park, Ph. D., Chairman, USAAhmed Derradji Aouat, Ph. D., Secretary, Canada
Baoshan Wu, ChinaShigeru Nishio, Ph. D., Japan
25th
ITTC, Fukuoka, Japan15 September 2008, 15:00 –
16:15
2
Outline
Introduction– Important concepts– ISO GUM (1995)
Membership & meetings
Procedures (5)– UA procedure
(revised)– Calibration Procedure– LDV Calibration– PIV Uncertainty– Resistance Tests
(revised)SummaryRecommendations
3
Important Concepts
Measurements traceable to a National Metrology Institute (NMI)Most uncertainty from data scatter in curve fit for conventional methods– Calibration data– Thrust coefficient versus advance ratio– Residual plot of data
Most uncertainty in naval hydrodynamics in repeatability of tests– Uncontrolled element in test– Resistance tests
4
Committee Members
Joel T. Park, Ph. D., Chair, NSWCCD, USAAhmed Derradji Aouat, Ph. D. Sec., IOT, CanadaErwan Jacquin, BEC, FranceBaoshan Wu, CSSRC, ChinaShigeru Nishio, Ph. D., Kobe U., Japan Wu Derradji Jacquin Park Nisho
5
Meetings
Bassin d’Essais des Carènes, Val-de-Reuil, France, March 30 - 31, 2006.China Ship Scientific Research Center, Wuxi, China, October 23 - 25, 2006.National Research Council Canada, Institute for Ocean Technology, St. John’s, Newfoundland, Canada, June 7 - 8, 2007.U. S. National Academy of Sciences, Naval Studies Board, Washington, DC, January 30 - February 1, 2008Kobe University, Kobe, Japan, September 12, 2008
6
Objectives of General Procedure
Simple and useable procedure tailored to ITTC hydrodynamics testingSpecific guidance on application of uncertainty to experimental naval hydrodynamicsSelf-contained without need for consultation with reference documentsITTC procedure derived from ISO Guide to the Expression of Uncertainty in Measurement (1995), referred to as the ISO GUM.
ITTC 7.5-02-01-01 (2008)
7
Uncertainty Analysis Fundamentals
Type A evaluation of standard uncertainty– Average or sample mean
– Sample variance
– Standard deviation, sx– Type A standard uncertainty definition or standard
deviation of the meanConventional statistical definitions: Ross (2004) p. 203, AIAA (1999) p. 7, ASME (2005) p. 6
∑=
>=<n
kkxnx
1
)/1(
∑=
><−−=n
kkx xxns
1
22 )()]1/(1[
nssu xxA /== ><
8
Uncertainty Analysis Fundamentals (cont.)
Type B evaluation of standard uncertainty– Previous measurement data
» Density, viscosity, and vapor pressure– Experience– Manufacturer’s specifications– Handbook– National Metrology Institute (NMI) traceable
calibration: NIST in USA, NMIJ in Japan, NMi in The Netherlands, NPL in UK, PTB in Germany, NRC in Canada, KRISS in ROK
9
Uncertainty Analysis Fundamentals (cont.)
Functional relationshipCombined uncertainty– Law of propagation of uncertainty– Sensitivity coefficient– Independent
– Correlated (weight set)
Expanded uncertainty– Coverage factor, k– Student t
∑=
∂∂=n
iiic xuxfyu
1
222 )()/()(
95%,2),(% === kykuU c
%tk =
),,,( 21 Nxxxfy K=
ii xfc ∂∂≡ /
∑∑==
≡=N
ii
N
iiic yuxucyu
1
2
1
22 )()]([)(
∑=
=N
iiic xucyu
1)()(
10
Relative Uncertainty Propeller
Reynolds number
Advance ratio
Thrust coefficient
)/(NDVJ =2222 )/()/()/(]/[ DuNuVuJu DNVJ −+−+=
)/( 42DNTKT ρ=
22
2222
)/(16)/(4
)/()/()/(]/[
DuNu
utTuKu
DN
tTTKT
−+−
+−∂∂+= ρρ
μρ /VDReD =
22
222
)/()/(
)/()/(]/)([
μ
ρ
μ
ρ
uDu
VuuReReu
D
VDDc
−+
++=
11
Numerical Evaluation of Sensitivity Coeff.
Central difference for uncertainty
Numerical sensitivity coefficient
Jitter program, Moffat (1982)
)],),(,,(),),(,,(][2/1[)(
1
1
Nii
Niiii
xxuxxfxxuxxfZyu
KK
KK
−−+==
)(/ iii xuZc =
12
Reporting Uncertainty Specific for U
Give full description of how measurand Y
was definedState measurement result as Y = y ± U– Give units of y
and U
Include relative expanded uncertainty U/|y|, |y|
≠ 0
Give values of k
and uc
(y)Give approximate level of confidence for the interval y ± U
and state how determined
Provide details or reference published document
13
Specification of Numerical Results
ms
= (100.021 47 ± 0.000 79) g, where the number following the symbol ± is the numerical value of U = kuc
(y), with U determined from uc
= 0.35 mg and k = 2.26 based on the t-distribution for ν = 9 degrees of freedom, and defines an interval estimated to have a level of confidence of 95 percent.
14
Other Elements of Procedure
Pre- & post-test uncertainty analysis– Uncertainty analysis in
data processing code
OutliersInter-Laboratory Comparisons– Youden plot
Special cases– Mass measurements– Instrument calibration
» NMI traceable» End-to-end or through
system calibration
– Repeat tests
15
Calibration Theory
Linear function– Independent variable,
x, calibration value set in engineering units
– Dependent variable, y, instrument response, usually in voltage units from A/D converter
Calibration value in post-processing code for engineering units
Uncertainty from theory of Scheffe (1973) & Carroll, et al. (1988)xxfy βα +== )(
ββαβα
/B,/AwhereByA/)y()y(fx
1=−=+=−==
ITTC 7.5-01-03-01 (2008)
16
Instrument Calibration Procedure
Calibration @ 10 approximately equal increments– System calibration with computer and software for test
measurements– Calculate mean and standard deviation for each point
on the order of 100 to 1000 points (5 to 50 s at 20 Hz sampling rate)
– Document» cutoff frequency» sample rate» number of samples
– NMI traceable reference standard with known uncertainty
17
Instrument Calibration Procedure (cont.)
Regression analysis of calibration data– Slope, intercept, correlation coefficient, standard error
of estimate, & outliers– Identify cause of outliers– Compute calibration uncertainty
Compare results to previous calibration– Hypothesis test of slope & intercept
Update computer slope & intercept3-point calibration check @ computer with test software
18
Uncertainty Elements for Instrument Cal.
Uncertainty in reference standard: NMI traceableUncertainty in curve fitType A uncertainty in data collection via computer for time series– Number of samples– Average– Standard deviation– Normally negligible: large values indication of
problem
19
Vertical Gyroscope Calibration in Roll
Reference Angle (deg)
-100-80 -60 -40 -20 0 20 40 60 80 100
A/D
Out
put (
V)
-10
-8
-6
-4
-2
0
2
4
6
8
10
Intercept: +0.0052 VSlope: -0.09143 V/degSEE: 0.0362 Vr: 0.999968
Linear RegressionIncreasing Roll AngleDecreasing Roll Angle
Reference Angle (deg)
-100-80 -60 -40 -20 0 20 40 60 80 100
Sta
ndar
dize
d R
esid
uals
-6
-4
-2
0
2
4
6
Intercept: -0.056 degSlope: -10.9370 deg/VSEE: 0.396 deg
Increasing Roll Angle Data Decreasing Roll Angle Data
Calibration Theory
20
Other Elements of Calibration
Hypothesis tests– Comparison with previous calibration results
Outliers– Chauvenet’s criteria– Standardized residuals
Force calibration– Mass uncertainty
Pulse count – optical encoders– Propeller shaft speed– Carriage speed
)1( wa ρρ /mgF −=
∑=
=n
iim uu
1
21
Equations for LDA Calibration
LDA optical calibration
Rotating disk calibration
Uncertainty equationsωπ rV 2=
22222 )2()2( ωππω uruu rV +=222 )/()/()/( ωωuruVu rV +=
fDD ffV δλθ == ]/)2/(sin2[
rVcrVc πωπω 2/,2/ 21 =∂∂==∂∂=
ITTC 7.5-01-03-02 (2008)
22
LDV Velocity Uncertainty
Axial LDA Velocity (m/s)0 5 10 15 20
U95
(m/s
)
0.000
0.005
0.010
0.015
0.020
0.025
0.030
Total Uncertainty for r = 50 mmRotational Velocity UncertaintyRadial UncertaintyLDA Noise
r = 100 mm
r = 50 mm
Bean & Hall (NIST, 1999)
07 May 2001
23
Comparison of Disk Results
Element NSWC NIST NMIJ PTB r 0.061 0.0074 0.0017 0.041fr 0.062 0.26 0.0018 0.035δf --- 0.16 --- ---Angle --- 0.011 0.017 0.0022fD 0.026 0.36 0.20 0.010Curve fit 0.043 --- --- ---Combined 0.10 0.48 0.20 0.055
Expanded Uncertainty in % @ 20 m/s
24
Particle Image Velocimetry (PIV)
Example of uncertainty analysis (UA) procedurePresent procedure developed from the guideline of Visualization Society of Japan recommendation (PIV-STD project, Nishio, et al., 1999)
uΔX/Δtu δα += )(Flow speed
Image displacement
Time interval
Magnification factor
ITTC 7.5-01-03-03 (2008)
25
Accumulation for Total Performance
Accumulation for total performance by the uncertainty for the flow speed
uu
, ux
, ut
: uncertainties of u, x and t
222c )/()/( tuuxuuuu txu ∂∂+∂∂+=
26
PIV Calibration Uncertainty
27
Summary of Uncertainty for Velocity uParame-
terCate-gory Error sources u(xi
) (unit) ci(unit) ci
u(xi
) (unit)
α Magnification Factor 0.00165 (mm/pix) 1580.0 (pix/s) 2.61
ΔX Image displacement 0.204 (pix) 132.0 (mm/ pix/s) 26.8
Δt Image interval 5.39E-09 (s) 1.2 (mm/s2) 6.47E-09
δu Experiment 0.732 (mm/s) 1.0 0.732
Combined uncertainty u 26.9 (mm/s)
26.80.204 (pix)
28
Summary of PIV Calibration Results
Total number of elements: 15– Magnification: 6– Displacement: 5– Time: 2– Velocity: 2
Velocity: 0.500 ±0.054 m/s (±11 %)
Dominant terms– Mis-matching: 26.4 mm/s
Secondary terms– Magnification: 2.6 mm/s– Sub-pixel
analysis: 4.0 mm/s– Laser power
fluctuation: 3.0 mm/s
29
Guidelines for UA in Resistance Tests
Data reduction equations– Total resistance coefficient– Form factor– Others: Re, Fr, frictional, & residuary – See procedure
Measurement system descriptionCalibration – See procedure for details– Force and mass– Resistance– Towing speed
30
Revised Procedure
Uncertainty Analysis in EFD, Guidelines forResistance Towing Tank Tests (1999)
Revise QM Procedure 7.5-02-01-02 (1999)
General Guidelines for Uncertainty Analysisin Resistance Towing Tank Tests (2008)
7.5-02-01-01 (2008)Guide to the Expression of
Uncertainty in Experi- mental Hydrodynamics
7.5-02-02-01 (2002)Resistance,
Resistance Test
7.5-01-03-01 (2008)Uncertainty Analysis -
Instrument Calibrations
ISO GUMISO GUM
AIAAAIAA5 pp
16 pp
31
UA in Resistance in Tow Tank Tests
Total resistance coefficient– Data reduction equation
– Uncertainty equation)/(2 2SVRC TT ρ=
222
22
)/()/()/2(
)]/)(/[()/(
SuRuVu
utCu
STRTV
tTCT
++
+∂∂= ρρ
ITTC 7.5-02-01-02 (2008)
32
Prohaska method
Intercept & its standard deviation from linear regression theoryExample from CSSRC– 0.1574±0.0097 (±6.2 %)
Additional terms from CF & CT at x
= 0
Form Factor
6410
1
<<≤
+=−
n.Fr
kC/bFrC/C Fn
FT
Fr4/CF
0.0 0.1 0.2 0.3 0.4 0.5 0.6 0.7
CT/
CF -
10.12
0.14
0.16
0.18
0.20
0.22
0.24
0.26
0.28
0.30
0.32
Slope: 0.1924k: 0.1574SEE: 0.0105r: 0.977
Linear Fit+/-95% Prediction Limit+/-95% Confidence Limit
Model Data
1FT −= C/Ck
33
Other Elements of Final Report
Terms of referenceUncertainty analysis symbolsOther activitiesHistory of uncertainty analysisRecommendation INC-1 (1980)Importance of uncertainty analysisRepeatability and reproducibility of data
34
Other Elements of Final Report (cont.)
Inter-laboratory comparisons– Youden plot
Free-running model tests– Instrument calibration– Model speed– Circle manoeuvres
Uncertainty of water propertiesUncertainty in PMM procedure
35
Recommendations
Adopt 2 revised and 3 new procedures from UACAdopt ISO (1995) as the UA standard for ITTC– Modify existing ITTC procedures to conform to ISO
(1995) by relevant committees with assistance of UAC– Adopt Annex J of ISO (1995) for ITTC symbols for
UA and VIM as dictionary– Include UA in benchmark data & review by UAC
Extend PIV procedure to include stereo PIV
36
Important Concepts
Measurements traceable to a National Metrology Institute (NMI)Most uncertainty from data scatter in curve fit for conventional methods– Calibration data– Thrust coefficient versus advance ratio– Residual plot of data
Most uncertainty in naval hydrodynamics in repeatability of tests– Resistance tests
37
Support Slides
Coleman & Steele on ISO (1995) - 5 slidesUncertainty analysis - 11 slidesCalibration data - 4 slidesLDV data - 1 slidePIV details on displacement & magnification uncertainties - 2 slidesResistance testing - 8 slidesRepeatability - 2 slidesYouden plot - 1 slide
38
Glenn Steele on ISO (1995)From: Glenn Steele [mailto:[email protected]] Sent: September 3, 2008 3:40 PM To: Derradji, Ahmed Cc: Hugh W. Coleman Subject: RE: 25th ITTC-Japan: Uncertainty Analysis Discussion
Ahmed,
I am responding to your phone call last week and the e-mail below. As I stated to you, Hugh Coleman and I agree that the ISO Guide is the international standard for uncertainty analysis. We state this in our book, Coleman and Steele (1999). We do not state that the guide is inappropriate for engineering experiments or tests, but instead point out the different definitions for uncertainty, Type A or B and systematic or random. Your statement below clearly summarizes my opinions expressed in our phone conservation - As far as I know, the ASME PTC 19.1 (2005) is in harmony with ISO GUM, and I think you and I agree that the ISO is the international organization, no questions. Uncertainty components types A and B of ISO-GUM look at the sources of uncertainty, while random and systematic uncertainty components of ASME PTC (2005) look at the effects of uncertainties on the test results. Ultimately, regardless what procedure one uses, the final standard uncertainty estimate should be the same.
If you have any other questions or need further clarification, please let me know.
Sincerely,
Glenn
39
Coleman & Steele (1999) on ISO (1995)
Coleman & Steele (1999) pp. 248 - 249
40
Coleman & Steele (1999) – cont.
41
ASME PTC 19.1-2005
Harmonization of this Supplement with the ISO GUM is achieved by encouraging subscripts with each uncertainty estimate to denote the ISO Type, i. e., using the subscripts of either “A” or “B.”
ASME (2005) p. 1
42
Other Adaptations of ISO (1995)
Taylor, B. N. and Kuyatt, C., 1994, “Guidelines for Evaluating and Expressing the Uncertainty of NIST Measurement Results”, NIST Technical Note 1297ASME PTC 19.1-2005, “Test Uncertainty”AIAA S-071A-1999, “Assessment of Experimental Uncertainty With Application to Wind Tunnel Testing
43
Recommendation INC-1 (1980)
Source: Working Group on the Statement of Uncertainties, Bureau International des Poids et Mesures (BIPM), http://www.bipm.org/Two categories of uncertainty– A. Those which are evaluated by statistical
methods for a series of observations– B. Those which are evaluated by other meansGiacomo (1981)
ISO (1995)
44
Recommendation INC-1 (1980) (cont.)
Category A characterization– Estimated variances– Number of degrees of freedom
Category B characterization– Approximation to corresponding variances
Combined uncertainty– Usual method for combination of variances– Uncertainty expressed as standard deviation
Overall uncertainty with stated factor
2is
iν
2iu
45
Expanded Uncertainty
Combined standard uncertainty, uc
(y): universal expression of measurement uncertaintyExpanded uncertainty, U: inclusion of large fraction of values– Coverage factor, k– Measurement result– Large interval
)(ykuU c=UyY ±=
UyYUy +≤≤−
46
Law of Propagation of Uncertainty
General law of propagation of uncertainty
General law for uncorrelated data ),()()(2
)()(
1
1 1
1
222
jijij
N
i
N
iji
N
iiic
xxrxuxucc
xucyu
∑ ∑
∑−
= +=
=
+=
0),( =ji xxr ∑=
=N
iiic xucyu
1
222 )()(
47
Correlated Input Quantities (cont.)
Special case for perfectly correlated data– Weight set for calibration of force
1),( +=ji xxr2
1
2 )()( ⎥⎦⎤
⎢⎣⎡= ∑
=
N
iiic xucyu
∑=
=N
iiic xucyu
1)()(
Flow Diagram for Jitter Program
Readxi , δ xi
Subroutinef = f(x1 ,…xi ,…, xN )
i = 1δ g = 0
Subroutineci = ¶ f/¶ xi
e = (δ xi ¶ f/¶ xi )2
δ g = δ g + e
i = i + 1
i < N
δ f = (δ g)1/2
Printf, δ f
Stop
Start Yes
No
Moffat (1982)
Flow Diagram for Subroutine ¶ f/¶ xi
Moffat (1982)
Return
Subroutineci = ¶ f/¶ xi
SubroutineF+ui = f(x1 ,...,xi +ui ,…, xN )F-ui = f(x1 ,...,xi -ui ,…, xN )
¶ f/¶ xi = (F+ui - F-ui )/(2ui )
50
Pre-Test Uncertainty Analysis
Data reduction program for processing data– Measurement equations– Uncertainty analysis
» Elemental uncertainty & relative importance» Combined & expanded uncertainty» Calibration factors for conversion to physical units» Type A & B estimates, for low noise instruments Type A
should be small relative to B
Planning and design of test– Selection of instrumentation for required uncertainty
results
51
Post-Test Uncertainty Analysis
Post-test data processing code same as pre-test, including uncertainty estimatesAll measurements NMI traceableUncertainty estimates from post-processing code suitable for inclusion in final reportComparison of pre-test and post-test uncertainty estimates– Post-test results consistent with pre-test estimates– Review for potential improvements and reduction of
uncertainty in future tests
52
Future of ISO (1995)
ISO (1995) to remain unchanged for near futureSupplements and other documents– Supplement 1: Propagation of distributions using a
Monte Carlo method (2008)– Supplement 2: Models with any number of output
quantities– Evaluation of measurement data –
An introduction to
the GUM– Evaluation of measurement data –
The role of
measurement uncertainty in conformity assessmentBIPM, Joint Committee for Guides in Metrology
http://www.bipm.org/en/committees/jc/jcgm/
53
Calibration Theory (cont.)
Uncertainty in calibration
Uncertainty in post-processed data
22221
2121
2 −− ==
++≤≤+−
N,N
xxxx
Fc,tcwhere)scc(See)x(fy)scc(See)x(f
Scheffe (1973)Carroll, Spiegelman, & Sacks (1988)
54
Columbia Transverse Acceleration Cal.
Reference Acceleration (g)-1.0 -0.5 0.0 0.5 1.0
Vol
tage
Out
put (
Vdc
)
-8
-6
-4
-2
0
2
4
6
8
Columbia SN 1649Intercept: -0.0847 VSlope: +7.9294 V/g4/27/05 H. W. Reynolds
Linear RegressionAccelerometer Data
Reference Acceleration (g)-1.0 -0.5 0.0 0.5 1.0
Acc
eler
atio
n R
esid
ual (
g)
-0.015
-0.010
-0.005
0.000
0.005
0.010
0.015
Columbia SN 1649Intercept: +0.0107 gSlope: +0.12611 g/V4/27/05 H. W. Reynolds
+/-95 % Confidence LimitAccelerometer Data
55
Tunnel Speed
Main Drive Motor Speed (rpm)0 10 20 30 40 50 60
Tunn
el V
eloc
ity (m
/s)
0
5
10
15
20
Linear FitLDA Data26 Oct 2000
y = a + bxa = -0.164 m/sb = 0.3199 m/s/rpmr = 0.999961
Main Drive Motor Speed (rpm)0 10 20 30 40 50 60
Vel
ocity
Res
idua
l (m
/s)
-0.10
-0.05
0.00
0.05
0.10
y = a + bxa = -0.164 m/sb = 0.3199 m/s/rpmr = 0.999961
LDA Data26 Oct 2000
56
Non-Linear Tunnel Speed
Main Drive Motor Speed (rpm)0 10 20 30 40 50 60
Vel
ocity
Res
idua
l (m
/s)
-0.10
-0.05
0.00
0.05
0.10
26 Oct 2000
Low Range, y = a + bxa = -0.1314b = 0.3231r = 0.999973
High Range, y = a + bxc
a = 0.0679b = 0.2749c = 1.0359r = 0.9999983
LDA Data, High RangeLDA Data, Low Range
+/-95 % Prediction Limit
57
LDV Calibration Data
Reference Velocity (m/s)
0 5 10 15 20
LDV
Vel
ocity
(m/s
)
0
5
10
15
20
y = a + bxa = 0.0007b = 0.98488r = 0.99999985SEE = 0.00286 m/s
Linear RegressionLDV Data 07 May 01
Reference Velocity (m/s)
0 5 10 15 20
Vel
ocity
Res
idua
l (m
/s)
-0.10
-0.08
-0.06
-0.04
-0.02
0.00
0.02
0.04
0.06
0.08
0.10
Intercept: -0.0007Slope: 1.01535Focal L: 1600 mmBeam Space: 115 mmWavelength: 514.5 nm
+/-95 % Prediction LimitLDV Data 07 May 01Outlier Data
58
Parame-ter
Cate-gory Error sources u(xi
) (unit) ci(unit) ci
u(xi
) uc
α(mm/pix)
Calibra-tion
Reference image 0.70 (pix) 3.84E-04 (mm/pix2) 2.69E-04
Physical distance 0.02 (mm) 1.22E-03 (1/pix) 2.44E-05
Image distortion by lens 4.11 (pix) 3.84E-04 (mm/pix2) 1.57E-03
Image distortion by CCD 0.0056 (pix) 3.84E-04 (mm/pix2) 2.15E-06
Board position 0.5 (mm) 2.84E-04 (1/pix) 1.42E-04
Parallel board 0.035 (rad) 0.011 (mm/pix) 3.85E-04 0.00165
Uncertainty Sources & Propagation: α
59
Uncertainty Sources & Propagation: ΔX
Parame- ter Category Error sources u(xi
) (unit) ci(unit) ci
u(xi
) uc
ΔX(pix)
Acquisi-tion
Laser power fluctuation 0.0071 (mm) 3.16 (pix/mm) .0224
Image distortion by CCD 0.0056 (pix) 1.0 0.0056
Normal view angle 0.035 (rad) 0.011 (mm/pix) 3.85E-04
Reduc-tion
Mis-matching error 0.20 (pix) 1.0 0.20
Sub-pixel analysis 0.03 (pix) 1.0 0.03 0.2040.204
0.20
60
Measurement System
61
Captive vs Free Running Model Tests
Captive Model Tests vs. Free Running Model Tests (1)
In narrow sense, they usually refer to two types of manoeuvring model tests
In general sense, Captive Model Tests: resistance test, open water test, oblique towing test, rotating arm test, PMM test, ….Free Running Model Tests: seakeeping test, free model test for manoeuvring,
62
Captive vs Free Running Model Tests – cont.
From the viewpoint of measurand, hydrodynamic measurement in ITTC can be grouped primarily in three (3) types:
Hydrodynamic forces/moments measurement,
e.g., in captive model tests
Field measurement,
e.g., wake flow, pressure distribution, wave profile
Motion measurement,
e.g., in seakeeping, free model tests for manoeuvring
Captive Model Tests vs. Free Running Model Tests (2)
63
Captive vs Free Running Model Tests – cont.
The main objective of Captive Model tests is to measure the hydrodynamic forces/moments in steady motion of given condition.
Captive Model Tests vs. Free Running Model Tests (3)
Take the resistance measurement as an example to provide a general guideline for Uncertainty Analysis of captive model tests based on the ISO GUM (1995), because
1) there is only one component force (the longitudinal forces, i.e., resistance) to be measured in resistance test and,
2) it is a task for the 25th ITTC-UAC to revise the QM Procedure 7.5-02-01-02 (1999) Uncertainty Analysis in EFD, Guidelines for Resistance Towing Tank Tests
64
Captive Model Test ProceduresState of art, UA in resistance tests before 25th ITTC
Five (5) QM procedures
7.5 - 02 - 01 - 02 (1999) 5 pagesUncertainty Analysis in EFD, Guidelines for Resistance Towing Tank Tests
Concise and excellent, but as general as policy for UA in resistance tests
7.5 - 02 - 02 - 02 (2002) 18 pagesUncertainty Analysis, Example for Resistance Test
7.5 - 02 - 02 - 03 (2002) 5 pagesUncertainty Analysis Spreadsheet for Resistance Measurements
7.5 - 02 - 02 - 04 (2002) 4 pagesUncertainty Analysis Spreadsheet for Speed Measurements
7.5 - 02 - 02 - 05 (2002) 5 pagesUncertainty Analysis Spreadsheet for Sinkage and Trim Measurements
7.5 - 02 - 02 - 06 (2002) 4 pagesUncertainty Analysis Spreadsheet for Wave Profile Measurements
Step-by-step process
with high operability
To be revised as UAC task
65
Details not in Revised Procedure
Revise QM Procedure 7.5-02-01-02 (1999)
General Guidelines for Uncertainty Analysis in Resistance Towing Tank Tests (2008)
in which, 1) Uncertainties related to extrapolation and full-scale
predictions are not taken into consideration and,2) Specific details not included such as turbulence
stimulation, drag of appendages, blockage and wall effect of tank, scaling effect on form factor, and etc.
66
New Details in Revised Procedure
Revise QM Procedure 7.5-02-01-02 (1999)
General Guidelines for Uncertainty Analysis in Resistance Towing Tank Tests (2008)
in which, special attention is given to1) Uncertainties related to geometry of ship model and,2) Uncertainties in data reduction, taking the form factor ( k) by
the Prohaska’s method, as a example, where the Linear Least Square method is used as in calibration data analysis.
These can be referenced by other captive model tests.
67
Future Revisions to Related Procedurs
Revise QM Procedure 7.5-02-01-02 (1999)
General Guidelines for Uncertainty Analysis in Resistance Towing Tank Tests (2008)
Noted: 1) In the near future, the researchers and engineering in towing tank
will still follow the QM procedures (7.5-02-02-02~~06) practically, because these procedures are developed by resistance specialists and can be performed in high operability. UAC have no desire or attempt to revise these five (5) procedures by themselves.
2) Revision of these five (5) procedures will be done by the specialists in resistance or the Resistance Committee (RC), where all the valuable papers on UA in resistance tests since 2002 will be reviewed.
68
Review of Other Draft Procedures by UACReview Draft ITTC Procedure and Guidelines-Forces and Moment Uncertainty Analysis, Example for Planar Motion Mechanism Test by the Manoeuvring Committee (MC) (2008)
Noted:1) Suggestions for improvements in PMM procedure noted in UAC final
reporta) Traceability of measurements to NMI (NIST in USA)b) Mass uncertainty correlated not uncorrelatedc) Terminology on calibration and acquisition is confusing –
Recommend following new UA procedure on calibrationd) Uncertainty in water temperature appears to be lowe) Clarification needed on computation of uncertainty from repeat testsf) Alternate approach on carriage speed uncertainty suggested.
69
Repeatability
Sequence Number
0 2 4 6 8 10 12 14 16
Wav
e Am
plitu
de (m
m)
170
180
190
200
210
220Senix Gage #6201 +/-11 mm
Average+/-95 % Confidence LimitWave Amplitude DataOutlier Data
Test Sequence Number
0 5 10 15 20 25
(V -
<V>)
/<V>
(%)
-0.15
-0.10
-0.05
0.00
0.05
0.10
0.15
Lab A: 2.0375 +/-0.0014 m/sLab B: 2.54903+/-0.00048 m/s
Lab A (2001)
Lab B (2006)+/-95% Confidence, A
+/-95 % Confidence, B
Carriage Speed Wave Amplitude
70
Open Water Dynamometer Results
J
0.0 0.5 1.0 1.5
K T, 1
0ΔK Q
-0.2
0.0
0.2
0.4
0.6
0.8
1.0
KT 4th Order PolynomialKQ 4th Order PolynomialKQ Data, 1000 rpm KT Data, 1000 rpm
10 May 2002
J
0.0 0.5 1.0 1.5
ΔK T
-0.04
-0.02
0.00
0.02
0.04+/-95 % Prediction Limit
KT, 1000 rpm, 10 May 2002All Historical Data
Donnelly and Park (2002)
71
Youden Plot for Turbine Meters
Lab F
Dirritti, et al. (1993)
72
Carl Friedrich GaussBorn 30 April 1777 in Brunswick, GermanyDied 23 Feb 1855 in Gottingen, GermanyPredicted position of Ceres in 1801 by least squaresDirector of Gottingen Observatory in 1807Least squares method from normal pdf in 1809Pioneer in measurement errorRanked with Archimedes, Newton, and Euler
ASME 2009 Fluids Engineering Division Summer Meeting
http://www.asmeconferences.org/FEDSM09/Conference Chair: Joel Park, Ph. D.
August 2-5, 2009Vail Cascade Resort and Spa
1300 Westhaven DriveVail, Colorado 81657-3890 USA
Call for PapersSymposium Abstracts 12/12/08
Forum Abstracts 02/13/09