USE OF RICIAN DISTRIBUTIONS TO PREDICT THE DISTRIBUTIONS OF ULTRASONIC FLAW SIGNALS IN THE PRESENCE OF BACKSCATTERED NOISE

Similar documents
THE USE OF ULTRASONIC FLAW AND NOISE MODELS IN DESIGNING

ULTRASONIC SIGNAL CHARACTERIZATIONS OF FLAT-BOTTOM HOLES IN

THE PRACTICAL APPLICATION OF GRAIN NOISE MODELS IN TITANIUM BILLETS AND FORGINGS

RECENT ADVANCES AND IMPLEMENTATIONS OF FLEXIBLE EDDY. RJ. Filkins, J.P. Fulton, T.e. Patton, and J.D. Young

MORPHOLOGICAL FILTERS: STATISTICAL EVALUATION AND

Enhancement of the POD of Flaws in the Bulk of Highly Attenuating Structural Materials by Using SAFT Processed Ultrasonic Inspection Data

MEASUREMENT OF RAYLEIGH WAVE ATTENUATION IN GRANITE USING

AUTOMATED EDDY CURRENT DETECTION OF FLAWS IN SHOT-PEENED

DEFECT CHARACTERIZATION IN THICK COMPOSITES BY ULTRASOUND. David K. Hsu and Ali Minachi Center for NDE Iowa State University Ames, IA 50011

THE MEASUREMENT AND ANALYSIS OF ACOUSTIC NOISE AS A RANDOM VARIABLE. Mechanical and Aerospace Missouri-Columbia 65203

EE 422G - Signals and Systems Laboratory

NUMERICAL MODELING OF AIR-COUPLED ULTRASOUND WITH EFIT. D. E. Chimenti Center of Nondestructive Evaluation Iowa State University Ames, Iowa, USA

A NEW APPROACH FOR THE ANALYSIS OF IMPACT-ECHO DATA

DEVEIDPMENT OF A PC-BASED SIGNAL PROCESSING UNIT FOR NONDESTRUCTIVE

CRACK SIZING USING A NEURAL NETWORK CLASSIFIER TRAINED WITH DATA OBTAINED FROM FINI1E ELEMENT MODELS

ULTRASONIC DETECTION OF CRACKS BELOW BOLTS IN AIRCRAFT SKINS

A TRUE WIENER FILTER IMPLEMENTATION FOR IMPROVING SIGNAL TO NOISE AND. K.W. Mitchell and R.S. Gilmore

FLEXURAL TORSIONAL GUIDED WAVE PIPE INSPECTION

Time and Frequency Domain Windowing of LFM Pulses Mark A. Richards

ULTRASONIC NDE OF THREE-DIMENSIONAL TEXTILE COMPOSITES

EVALUATION OF MICROWAVE METHODS FOR THICKNESS MEASUREMENTS OF UQUID SHIM MATERIAL

OPTIMIZATION OF THE DELTA TECHNIQUE AND APPLICATION TO THE EVALUATION OF ELECTRON- BEAM WELDED TITANIUM AIRCRAFT PARTS

Emerging NDE Technology for Aging Aircraft

EFFECT OF SURFACE COATINGS ON GENERATION OF LASER BASED ULTRASOUND

EXPERIMENTAL GENERATION OF LAMB WAVE DISPERSION USING FOURIER

OPTIJvIAL ULTRASONIC FLAW DETECTION USING A FREQUENCY DIVERSITY TECHNIQUE ** Jafai Saniie, Tao Wang and Nihat M. Bilgutay*

ULTRASONIC DEFECT DETECTION IN BILLET USING TIME- OF-FLIGHT OF BOTTOM ECHO

USE OF A CHIRP WAVEFORM IN PULSED EDDY CURRENT CRACK DETECTION

REAL-TIME B-SCAN ULTRASONIC IMAGING USING A DIGITAL PHASED. Robert Dunki-Jacobs and Lewis Thomas General Electric Company Schenectady, New York, 12301

Measurement of phase velocity dispersion curves and group velocities in a plate using leaky Lamb waves

ULTRASONIC METHODS FOR DETECTION OF MICRO POROSITY IN COMPOSITE MATERIALS

G. Hughes Department of Mechanical Engineering University College London Torrington Place London, WClE 7JE, United Kingdom

Research on An Inspection Method for De-bond Defects in Aluminum. Skin-Honeycomb Core Sandwich Structure with Guided Waves

HANDBOOK OF NONDESTRUCTIVE EVALUATION (NDE) CAP ABILITY AND RELIABILITY*

ULTRASONIC SIGNAL PROCESSING TOOLBOX User Manual v1.0

Optimal matched filter design for ultrasonic NDE of coarse grain materials

A NOVEL HIGH SPEED, HIGH RESOLUTION, ULTRASOUND IMAGING SYSTEM

Effect of coupling conditions on ultrasonic echo parameters

MICROWAVE SCATTERING FOR THE CHARACTERIZATION OF A DISC-SHAPE VOID IN DIELECTRIC MATERIALS AND COMPOSITES

RELIABILITY OF GUIDED WAVE ULTRASONIC TESTING. Dr. Mark EVANS and Dr. Thomas VOGT Guided Ultrasonics Ltd. Nottingham, UK

LASER GENERATION AND DETECTION OF SURFACE ACOUSTIC WAVES

USING A SQUIRTER TO PERFORM PULSE-ECHO ULTRASONIC INSPECTIONS OF GAS TURBINE ENGINE COMPONENTS: THE PROS AND CONS. David A. Stubbs

AN ACTIVELY-STABILIZED FIBER-OPTIC INTERFEROMETER FOR

ON FIBER DIRECTION AND POROSITY CONTENT USING ULTRASONIC PITCH-CATCH TECHNIQUE IN CFRP COMPOSITE SOLID LAMINATES

USE OF GUIDED WAVES FOR DETECTION OF INTERIOR FLAWS IN LAYERED

EVALUATION OF INTERFACE IN CO-EXTRUDED ZIRCONIUM TUBE

MODELLING ULTRASONIC INSPECTION OF ROUGH DEFECTS. J.A. Ogilvy UKAEA, Theoretical Physics Division HARWELL Laboratory. Didcot, Oxon OXll ORA, U.K.

Spectral Distance Amplitude Control for Ultrasonic Inspection of Composite Components

FIRST MEASUREMENTS FROM A NEW BROADBAND VIBROTHERMOGRAPHY MEASUREMENT SYSTEM

AIP (2015) 34. AIP ISBN

THERMAL WA VB IMAGING OF AIRCRAFT STRUcruRES

THE ANALYSIS OF ADHESIVE BONDS USING ELECfROMAGNETIC

AN ADAPTIVE MORPHOLOGICAL FILTER FOR DEFECT DETECTION IN EDDY

R. D. Huber and G. H. Thomas

RADAR INSPECTION OF CONCRETE, BRICK AND MASONRY STRUCTURES

transient AI D converter Dio channel oscilloscope Tek 7704 peak/time recelver ~ (damping) trigger inspection plan 1/0

SCATTERING INDUCED ATTENUATION OF ULTRASONIC BACKSCATTERING. Department of Welding Engineering The Ohio State University Columbus, OR 43210

REAL-TIME X-RAY IMAGE PROCESSING; TECHNIQUES FOR SENSITIVITY

Ultrasonic pulse propagation in a bonded three-layered structure

NONLINEAR C-SCAN ACOUSTIC MICROSCOPE AND ITS APPLICATION TO CHARACTERIZATION OF DIFFUSION- BONDED INTERFACES OF DIFFERENT METALS

Non-Destructive Method Based on Rayleigh-Like Waves to Detect Corrosion Thinning on Non- Accessible Areas

Standard Practice for Ultrasonic Examination of Turbine and Generator Steel Rotor Forgings 1

DETECTION OF SUB LAYER FATIGUE CRACKS UNDER AIRFRAME RIVETS

A COMPACT EMAT RECEIVER FOR ULTRASONIC TESTING AT ELEVATED TEMPERATURES* L. R. Burns, G. A. Alers, and D. T. MacLauchlan

EDDY-CURRENT IMAGING FOR DEFECT CHARACTERIZATION. David. C. Copley. General Electric Company Aircraft Engine Business Group Evendale, OR 45215

MICROWAVE THICKNESS MEASUREMENTS OF MAGNETIC COATINGS. D.D. Palmer and V.R. Ditton

THEORETICAL SUMMARY Nonspecular acoustic beam refiection can be treated by the Complex-Source-

NARROWBAND ULTRASONIC SPECTROSCOPY FOR NDE OF LAYERED STRUCTURES T. Stepinski and M. Jonsson 1 Uppsala University, Uppsala, Sweden

Multi-Mode and Multi-Frequency Differential Lamb Wave Imaging with in situ Sparse Transducer Arrays

AIR-GAP DETECTION IN DIELECTRIC MATERIALS BY A STEP-FREQUENCY MICROWAVE TECHNIQUE

NONDESTRUCTIVE EVALUATION OF CLOSED CRACKS USING AN ULTRASONIC TRANSIT TIMING METHOD J. Takatsubo 1, H. Tsuda 1, B. Wang 1

Attenuation dependent detectability at ultrasonic inspection of copper

ACOUSTO-ULTRASONIC EVALUATION OF HYBRID COMPOSITES USING

2010 ULTRASONIC BENCHMARKS

DETECTION AND SIZING OF SHORT FATIGUE CRACKS EMANATING FROM RIVET HOLES O. Kwon 1 and J.C. Kim 1 1 Inha University, Inchon, Korea

ULTRASONIC MEASUREMENT SYSTEM FOR THE ASSESSMENT OF

3D Ultrasonic Imaging by Cone Scans and Acoustic Antennas

MULTI-PARAMETER ANALYSIS IN EDDY CURRENT INSPECTION OF

A Method for Quantitative Analysis of Transient Eddy Current Testing

A NON-CONTACT LASER-EMAT SYSTEM FOR CRACK AND HOLE

DAMAGE DETECTION IN PLATE STRUCTURES USING SPARSE ULTRASONIC TRANSDUCER ARRAYS AND ACOUSTIC WAVEFIELD IMAGING

FATIGUE CRACK DETECTION IN METALLIC MEMBERS USING SPECTRAL

Characterization of Damages in Honeycomb Structures Using SonatestDryScan 410D

STUDY ON SAW ATTENUATION OF PMMA USING LASER ULTRASONIC

Ripple and Uniformity Measurement of a Phased-Array Testing-Machine for round-bar Testing

CRACK PARAMETER CHARACTERIZATION BY A NEURAL NETWORK

Non-Contact Ultrasound Characterization of Paper Substrates

Application of Ultrasonic Guided Waves for Characterization of Defects in Pipeline of Nuclear Power Plants. Younho Cho

Optimized Semi-Flexible Matrix Array Probes for Large Rotor Shafts and DGS Sizing Diagram Simulation Tool

High contrast air-coupled acoustic imaging with zero group velocity Lamb modes

Ultrasonic Imaging of Tight Crack Surfaces by Backscattered Transverse Wave with a Focused Transducer

ULTRASONIC FIELD RECONSTRUCTION FROM OPTICAL INTERFEROMETRIC

THE LONG RANGE DETECTION OF CORROSION IN PIPES USING LAMB WAVES

A PHASED ARRAY ULTRASONIC TESTING OF A MANUAL THICK AUSTENITIC WELD FEEDBACK

ULTRASONIC DETECTION OF FATIGUE CRACKS BY THERMO-OPTICAL

INSPECTION OF COMPONENTS HA VING COMPLEX GEOMETRIES. Andrew D. W. McKie and Robert C. Addison, Jr.

PRACTICAL APPLICATION OF STATE-OF-THE-ART NDE TECHNIQUES: EVALUATION OF GRAPHITE-EPOXY COMPOSITE WING COVERS. Patrick H. Johnston and Doron Kishoni

S. GURESH 4 JAN 2017 S. JOHNSON 4 JAN 2017

COMPUTER MODELING OF EDDY CURRENT TRANSMIT-RECEIVE PROBES FOR. S.P. Sullivan, V.S. Cecco, L.S. Obrutsky, D. Humphrey, S.P. Smith and K.A.

Y. Li and R. B. Thompson Ames Laboratory Iowa State University Ames, Iowa 50011

Transcription:

USE OF RICIAN DISTRIBUTIONS TO PREDICT THE DISTRIBUTIONS OF ULTRASONIC FLAW SIGNALS IN THE PRESENCE OF BACKSCATTERED NOISE I. Valda, F. 1. Margetan, and R. B. Thompson Center for NDE Iowa State University 1915 Scholl Road Ames, IA 50011 INTRODUCTION In assessing the probability of detection (POD) of flaws during ultrasonic inspection, one needs to know the distribution of signal strengths that would be produced by flaws of the same nominal size [1]. Several factors contribute to creating such a distribution, including variations in flaw morphology, variations in the position of the flaw with respect to the insonifying beam, modifications of the beam by the microstructure, and the interaction between the flaw signal and noise signal backscattered from microstructural inhomogeneities. This paper deals with the latter mechanism, developing models which predict the distribution of signal in the presence of noise in terms of independent measures of the noise and the noise free flaw response. In its most elementary form, the problem is illustrated by the addition of a noise free signal, So, and a noise signal, Nr/ B Elementary trigonometry shows that, if 9 is a uniformly distributed random variable, and S = So + Nr/ B In agreement with intuition, <S>ISo approaches unity for high signal-to-noise (SNR) ratios and <S> approaches N 2 for low signal-to-noise ratios. A more sophisticated analysis has been developed in the radar and communication communities [2]. Considering a process in which signal and noise add linearly (as in the above example), and assuming, normally distributed noise and envelope detection, it has been shown that the resulting distribution has the following form (1) (2) Review of Progress in Quantitative Nondestructive Evaluation, Vol17 Edited by D.o. Thompson and D.E. Chimenti, Plenum Press, New York, 1998 105

fir) A =0 --~~----~~~~----------~------~~----~r o o Figure 1 A sketch of the Rician distribution for three signal-to-noise ratios. known as the Rician distribution. Here, A is the noise free envelope of the signal, a is the standard deviation of the noise, and 10 is the modified Bessel function of the first kind and zero order. Figure I sketches this function. When A=O, it has the form of the Rayleigh distribution while, when A2/2cf» 1 (high SNR), it approaches a normal distribution centered on A. In this paper, we consider the degree to which the Rician distribution is applicable to an ultrasonic inspection situation in which the signal is broadband, the noise may be neither white nor normally distributed, and gated peak-to-peak detection is used. The latter is selected because of its importance in industry, such as in the inspection of titanium billet material from which the rotating components of aircraft engines are fabricated [3]. DIRECT COMPARISON OF GATED, PEAK-TO-PEAK SIGNALS TO RICIAN DISTRIBUTION To ascertain the degree to which the Rician distribution is applicable to the ultrasonic case, an empirical study was conducted in which a scaled broadband "signal" was added to each of 252 noise waveforms taken from a Ti-17 sample at a selected time. The noise characteristics of this sample (AI) have been discussed elsewhere [4]. The "signal" was taken to be a reflection from a planar surface, scaled in accordance with the defmition where Vpp represents the peak-to-peak voltage within the gate. Insonification was with a 5 MHz, 0.74 in. diameter, 7.85 in. geometrical focal length probe. For various values of X, the scaled reference was added to each of the 252 noise waveforms, the peak-to-peak value of the superimposed waveforms within the gate was recorded, and a histogram of the result was constructed. These histograms were compared to the Rician distribution, where A was taken to be the peak-to-peak signal amplitude and a the rms noise level, as determined previously [4]. For the case of an 0.75 gate selected near the focal plane of the transducer, Figure 2 shows the results for X=O.I, 1, and 10. Note from Eqn. (3) that X is a noise-to-signal ratio, so high values of X correspond to low values of SNR. Examination of Figure 2 shows that agreement between the Rician distribution and the empirical distributions appears reasonable at high SNR (X=O.I), but that there is obviously a problem at low SNR (X=lO). (3) 106

Sla--_..,.,. S9*+-HoIM dialrtluuon. TI-17 A1 : PO, 1 T\.17 A1:,1 _0 -. -~,...- - ~,.»0r------------------------. ~.r---------------------~ (a) (b) ~.NoIM dilatrlbuuona fl.17.1:.-100.. ~0r-------~------------, 0.. (c) Figure 2 Comparison of Rician distribution to empirically determined distributions of signal and noise in Ti-l7. Gate width = 0.75 J.lsec. (a) x = O.l ; (b) x = 1.0; (c) x = to.o. 450 300 0 Sig.al+Noise distributions in ESaW gate T~17 A1 :.=10 0 0 Histogram 0 0 Riclan Fit 0 H(r') 150 00 +---------+--o<~~----- 000 005 r' 010 Figure 3 Comparison of Rician distribution to empirically determined distributions of signal and noise in Ti-17. Gate width = 0.185 J.lsec and x = to.o. 107

In assessing the possible causes of this difficulty, it was postulated that the length of the gate was playing an important factor. For sufficiently low SNR, one is essentially looking at the noise only. Margetan has shown that the distribution of gated peak-to-peak noise can be modeled by taking twice the maximum value of N independent samples of the distribution which governs the noise envelope observed at an instant of time [5]. N is determined by the ratio of the gate width and the equivalent square wave (ESQ) duration of the input pulse and can be thought of as the number of times that the noise assumes independent values within the gate. For the case under consideration, the ESQW duration of the input pulse was 0.185 flsec. Figure 3 shows the improved agreement for X=lO when the signal-plus-noise was sampled in such a gate. EXTENDED RICIAN MODEL FOR GATED PEAK-TO-PEAK DETECTION Based on these results, an extended Rician model has been developed. As illustrated in Figure 4, the total time gate is divided into a set of intervals whose length is the duration of the ESQW. In constructing the gated peak-to-peak noise model discussed above, one constructed the distribution by independently sampling the instantaneous noise envelope distributions in each of the intervals. The gated peak-to-peak noise distribution was then determined by a histogram of the maximum of these sampled distributions. For the signal-plus-noise case, the same basic idea is used. However, in one of the time intervals, the distribution of signal-plus-noise replaces the noise distribution. In our first implementation of this idea, it was assumed that the underlying statistics governing the instantaneous noise was normal. Figure 4 independent. I time gate I I I I + + ESQW I Gate divided into intervals in which signal and noise can be considered to be Then the noise envelope governed by the Rayleigh distribution, was independently sampled in all but one interval. In the remaining interval, the Rician distribution was sampled, based on the procedures described in the previous section. Again, the maximum value for all intervals was selected. Note that, for low SNR, this reduces to the procedure previously employed for noise only. For high SNR, this reduces to a simple Rician distribution, since the maximum will nearly always fall in the interval selected to represent the signal. Figures 5-7 represent the fit of this modified Rician distribution to data on 3 samples, obtained by the procedures discussed previously with a gate width of 0.75Ilsec. Figure 5 contains the data previously discussed to Ti-17 sample AI. Figure 6 contains results for Ti-64 sample KI. Figure 7 contains results for a stainless steel sample. Although no statistical measures of degree of fit have been employed, it is evident that the fit is much better for this extended Rician than for the simple Rician, particularly for low SNR. 108

lo. SJgnal+Noise dd:tributlom 11-17 A1 : :1""0.'\.. ~------,-~-."." l ". "" Slg "'1I_1oM 1\.\7 ",: ~,.O "'- - """'-." 010 003 SigIYl+ NoIse dii!.tl.bulloo!i Ti-t1 M : r1gg o _ -. Ho.. (a) (b) (c) Figure 5 Comparison of extended Rician distribution to empirically determined distributions of signal and noise in Ti-17. Gate width = 0.75I-1sec. (a) x = 0.1; (b) x = 1.0; (c) x = 10.0. " Slgf\l.l+Nocw dlstribu'\ic)ns 'JI.64 Kt: 11:"'0.1,., StgnaHNOIIH da1uoo\.ons r.. 6of Kl ~ :1""1.0 O)a..,,.,,.. =_- -1. 001) Sigl\ll.~ dl'slflbulions n.64 K1 : x.'0.0.. L--""''-- ~ _.. - Q.-.cIA.c..M1 Cit! (a) (b) (c) Figure 6 Comparison of extended Rician distribution to empirically determined distributions of signal and noise in Ti-6AI-4V. Gate width = 0.75I-1sec. (a) x = 0.1; (b) x = 1.0; (c) x = 10.0. 109

Signal+No[se distributions Stainless St~t!t x~o _1 Signal+Noise distributions Stainms Steel: x:1.0 200r-.----------------------------, 300r-------------------------------, b 150 " " " ~ 100 '00.0 00 O' D. o. 00 07 000 005 0,0 0.. 300 S;gnal+NoIse distributions Stainless Steel: ""10.0 "., " _ GM"'~ ~==1 200 C :r '.0 00 000 005 0'0 0', Figure 7 Comparison of extended Rician distribution to empirically determined distributions of signal and noise in stainless steel Gate width = 0.75 flsec. (a) x = 0.1; (b) x = 1.0; (c) x = 10.0. 110

18.,.. Signllt+Noise distributions lor SHA'5 Slgnal+Nolso dis'ribu'lons lor SHA *3 \-~ Eo I dit.arom "C M~ _Vpo ". ". c r I. 0 s b 00 DO 02 O. O..0 o. 02 0'.' Signal+_ distributions Slgnal+NoIse dislributions lor SHA for SHAI2 '8.,.. aiii.. 1ibIn I W_uredVpp 120 l- a...-/ o ~uredv~ 12. C r,. 10.0 '0 D. 02 00., c DO d 0, 0' Figure 8 Comparison of extended Gaussian distribution to experimentally observed signals of synthetic hard-alpha inclusions of various sizes (diameter=height). (a) #2; (b) #3; (c) #4; (d) #5. Our final initial test of this approach made use of experimental waveforms obtained on a sample containing 8, nominally identical synthetic hard-alpha inclusions of each of the sizes #2, #3, #4, and #5 [6]. In Figure 8, the fitted Rician is plotted as the solid line. The individual peak-topeak values are indicated by the square symbols plotted along the abscissa. In the development of the Rician distribution, cr was deduced from experimental measurements of the noise distribution and A was predicted theoretically [6]. The agreement is not quite as good as for the previously presented results, in part because of some significant outliers. It is possible that these might be a consequence of fabrication errors. In any case, we consider the results to be quite encouraging for a first attempt with no adjustable parameters. CONCLUSIONS An extended Rician model for the distribution governing gated peak-to-peak detection of signal in the presence of noise has been developed and compared to experimental data. The initial comparisons are quite favorable. Future work involves considerably more experimental validation, including the effects of greater gate widths, with model modifications perhaps required as a result of those comparisons. ACKNOWLEDGEMENT This work was supported by the Engine Titanium Consortium under the Federal Aviation Administration Grant No. 94-G-048. III

REFERENCES 1. W. D. Rummel, G. L. Hardy, and T. D. Cooper, "Applicability ofnde Reliability to Systems", in Metals Handbook, Ed. 9, Vol. 17, Nondestructive Evaluation and Quality Control (ASM, Metals Park, QH, 1989), pp. 674-684. 2. M. Schwartz, Information Transmission, Modulation and Noise (McGraw-Hill, NY, 1980), pp.377-382. 3. E. 1. Nieters, R. S. Gilmore, R. C. Trzaskos, J. D. Young, D. C. Copley, P. 1. Howard, M. E. Keller, and W. 1. Leach, "A Multizone Technique for Billet Inspection", in Review of Progress in Quantitative Nondestructive Evaluation, Vol. 14, D. Q. Thompson and D. E. Chimenti, eds. (Plenum Press, NY, 1995), pp. 2137-2144. 4. 1. Yalda, F. J. Margetan, K. Y. Han, and R. B. Thompson, "Survey of Ultrasonic Grain Noise Characteristics in Jet Engine Alloys", in Review of Progress in Ouantitative Nondestructive Evaluation, Vol. 15, D. Q. Thompson and D. E. Chimenti, eds. (Plenum Press, NY, 1996), pp. 1487-1494. 5. F. 1. Margetan, I. Yalda, and R. B. Thompson, "Predicting Gated-Peak Grain Noise Distributions for Ultrasonic Inspections of Metals", in Review of Progress in Quantitative Nondestructive Evaluation, Vol. 15, D. Q. Thompson and D. E. Chimenti, eds. (Plenum Press, NY, 1996), pp. 1509-1516. 6. C.-P. Chiou, F. J. Margetan, R. B. Thompson, "Modeling of Ultrasonic Signals from Weak Inclusions", in Review of Progress in Quantitative Nondestructive Evaluation, Vol. 15, D. O. Thompson and D. E. Chimenti, eds. (Plenum Press, NY, 1996), pp. 49-55. 112