| Year |
Citation |
Score |
| 2020 |
Fujiwara GEC, Bragg MB, Broeren AP. Comparison of Computational and Experimental Ice Accretions of Large Swept Wings Journal of Aircraft. 57: 342-359. DOI: 10.2514/1.C035631 |
0.816 |
|
| 2019 |
Fujiwara GEC, Bragg MB. Method for Designing Three-Dimensional Swept Hybrid Wings for Icing Wind-Tunnel Tests Journal of Aircraft. 56: 730-746. DOI: 10.2514/1.C035136 |
0.513 |
|
| 2019 |
Fujiwara GEC, Bragg MB. Method for Designing Hybrid Airfoils for Icing Wind-Tunnel Tests Journal of Aircraft. 56: 137-149. DOI: 10.2514/1.C034987 |
0.575 |
|
| 2016 |
Ansell PJ, Bragg MB. Unsteady modes in flowfield about airfoil with horn-ice shape Journal of Aircraft. 53: 475-486. DOI: 10.2514/1.C033421 |
0.78 |
|
| 2016 |
Camello SC, Lee S, Lum C, Bragg MB. Generation of fullspan leading-edge 3D ice shapes for swept-wing aerodynamic testing 8th Aiaa Atmospheric and Space Environments Conference. |
0.601 |
|
| 2015 |
Diebold JM, Bragg MB. Wake-survey technique for Iced swept-wing aerodynamics Aiaa Journal. 53: 1712-1719. DOI: 10.2514/1.J053774 |
0.555 |
|
| 2015 |
Ansell PJ, Bragg MB. Characterization of low-frequency oscillations in the flowfield about an iced airfoil Aiaa Journal. 53: 629-637. DOI: 10.2514/1.J053206 |
0.769 |
|
| 2014 |
Ansell PJ, Bragg MB. Measurement of unsteady flow reattachment on an airfoil with an ice shape Aiaa Journal. 52: 656-659. DOI: 10.2514/1.J052519 |
0.731 |
|
| 2014 |
Ansell PJ, Kerho MF, Bragg MB. Application of a hinge-moment-based envelope protection system on a wing Journal of Aircraft. 51: 2038-2042. DOI: 10.2514/1.C032703 |
0.668 |
|
| 2014 |
Ansell PJ, Bragg MB. Unsteady modes in the flowfield about an airfoil with a horn-ice shape 44th Aiaa Fluid Dynamics Conference. |
0.765 |
|
| 2013 |
Fujiwara GEC, Woodard BS, Wiberg BD, Mortonson AJ, Bragg MB. A hybrid airfoil design method for icing wind tunnel tests 5th Aiaa Atmospheric and Space Environments Conference. DOI: 10.2514/6.2013-2826 |
0.508 |
|
| 2013 |
Diebold JM, Broeren AP, Bragg MB. Aerodynamic classification of swept-wing ice accretion 5th Aiaa Atmospheric and Space Environments Conference. DOI: 10.2514/6.2013-2825 |
0.808 |
|
| 2013 |
Broeren AP, Potapczuk MG, Riley JT, Villedieu P, Moëns F, Bragg MB. Swept-wing ice accretion characterization and aerodynamics 5th Aiaa Atmospheric and Space Environments Conference. DOI: 10.2514/6.2013-2824 |
0.822 |
|
| 2013 |
Campbell SE, Bragg MB, Neogi NA. Fuel-optimal trajectory generation for persistent contrail mitigation Journal of Guidance, Control, and Dynamics. 36: 1741-1750. DOI: 10.2514/1.55969 |
0.516 |
|
| 2013 |
Ansell PJ, Bragg MB. Characterization of ice-induced low-frequency flowfield oscillations and their effect on airfoil performance 31st Aiaa Applied Aerodynamics Conference. |
0.807 |
|
| 2013 |
Ansell PJ, Kerho MF, Bragg MB. Envelope protection for contaminant-induced adverse aerodynamics on a wing using flap hinge moment measurements 31st Aiaa Applied Aerodynamics Conference. |
0.675 |
|
| 2013 |
Diebold JM, Bragg MB. Study of a swept wing with leading-edge ice using a wake survey technique 51st Aiaa Aerospace Sciences Meeting Including the New Horizons Forum and Aerospace Exposition 2013. |
0.541 |
|
| 2013 |
Monastero MC, Bragg MB. Validation of 3-D ice accretion measurement methodology using pressure-sensitive paint Transactions of Japanese Society For Medical and Biological Engineering. 51. |
0.597 |
|
| 2013 |
Fujiwara GEC, Wiberg BD, Woodard BS, Bragg MB. 3D swept hybrid wing design method for icing wind tunnel tests Transactions of Japanese Society For Medical and Biological Engineering. 51. |
0.485 |
|
| 2013 |
Wiberg BD, Fujiwara GEC, Woodard BS, Bragg MB. Large-scale swept-wing icing simulations in the NASA glenn icing research tunnel using LEWICE3D Transactions of Japanese Society For Medical and Biological Engineering. 51. |
0.597 |
|
| 2012 |
Ansell PJ, Bragg MB. Measurement of unsteady flow reattachment on an airfoil with a leading-edge horn-ice shape 30th Aiaa Applied Aerodynamics Conference 2012. 611-624. |
0.777 |
|
| 2012 |
Diebold JM, Monastero MC, Bragg MB. Aerodynamics of a swept wing with ice accretion at low Reynolds number 30th Aiaa Applied Aerodynamics Conference 2012. 591-610. |
0.548 |
|
| 2011 |
Ansell PJ, Bragg MB, Kerho MF. Envelope protection system for iced airfoils using flap hinge moment Sae Technical Papers. DOI: 10.4271/2011-38-0066 |
0.806 |
|
| 2011 |
Ansell PJ, Bragg MB, Kerho MF. Stall warning using flap hinge moment measurements Journal of Aircraft. 48: 1822-1824. DOI: 10.2514/1.C031435 |
0.681 |
|
| 2010 |
Broeren AP, Whalen EA, Busch GT, Bragg MB. Aerodynamic simulation of runback ice accretion Journal of Aircraft. 47: 924-939. DOI: 10.2514/1.46475 |
0.85 |
|
| 2010 |
Broeren AP, Bragg MB, Addy HE, Lee S, Moens F, Guffond D. Effect of high-fidelity ice-accretion simulations on full-scale airfoil performance Journal of Aircraft. 47: 240-254. DOI: 10.2514/1.45203 |
0.871 |
|
| 2010 |
Ansell PJ, Bragg MB, Kerho MF. Envelope protection system using flap hinge moment measurements 28th Aiaa Applied Aerodynamics Conference. |
0.734 |
|
| 2009 |
Busch GT, Bragg MB. Experimental study of full-scale iced-airfoil aerodynamic performance using sub-scale simulations 1st Aiaa Atmospheric and Space Environments Conference. |
0.879 |
|
| 2009 |
Campbell SE, Neogi NA, Bragg MB. An operational strategy for persistent contrail mitigation 9th Aiaa Aviation Technology, Integration and Operations (Atio) Conference, Aircraft Noise and Emissions Reduction Symposium (Aners). |
0.477 |
|
| 2008 |
Busch GT, Broeren AP, Bragg MB. Aerodynamic simulation of a horn-ice accretion on a subscale model Journal of Aircraft. 45: 604-613. DOI: 10.2514/1.32338 |
0.846 |
|
| 2008 |
Whalen EA, Broeren AP, Bragg MB. Aerodynamics of scaled runback ice accretions Journal of Aircraft. 45: 591-603. DOI: 10.2514/1.32274 |
0.867 |
|
| 2008 |
Campbell SE, Neogi NA, Bragg MB. An optimal strategy for persistent contrail avoidance Aiaa Guidance, Navigation and Control Conference and Exhibit. |
0.461 |
|
| 2008 |
Broeren AP, Bragg MB, Addy HE, Lee S, Moens F, Guffond D. Effect of high-fidelity ice accretion simulations on the performance of a full-scale airfoil model 46th Aiaa Aerospace Sciences Meeting and Exhibit. |
0.836 |
|
| 2007 |
Broeren AP, Busch GT, Bragg MB. Aerodynamic fidelity of ice accretion simulation on a subscale model Sae Technical Papers. DOI: 10.4271/2007-01-3285 |
0.87 |
|
| 2007 |
Campbell SE, Broeren AP, Bragg MB. Sensitivity of aircraft performance to icing parameter variations Journal of Aircraft. 44: 1758-1760. DOI: 10.2514/1.32355 |
0.859 |
|
| 2007 |
Jacobs JJ, Bragg MB. Two- and three-dimensional iced airfoil separation bubble measurements by particle image velocimetry Collection of Technical Papers - 45th Aiaa Aerospace Sciences Meeting. 2: 1022-1037. |
0.656 |
|
| 2007 |
Campbell SE, Broeren AP, Bragg MB, Miller DR. Aircraft performance sensitivity to icing cloud conditions Collection of Technical Papers - 45th Aiaa Aerospace Sciences Meeting. 2: 989-1005. |
0.826 |
|
| 2006 |
Broeren AP, Bragg MB, Addy HE. Flowfield measurements about an airfoil with leading-edge ice shapes Journal of Aircraft. 43: 1226-1234. DOI: 10.2514/1.19021 |
0.837 |
|
| 2006 |
Jacobs JJ, Bragg MB. Particle image velocimetry measurements of the separation bubble on an iced airfoil Collection of Technical Papers - Aiaa Applied Aerodynamics Conference. 3: 1894-1907. |
0.593 |
|
| 2006 |
Broeren AP, Bragg MB. Aerodynamics of ice remnants from protected surfaces Collection of Technical Papers - 44th Aiaa Aerospace Sciences Meeting. 5: 3149-3169. |
0.837 |
|
| 2006 |
Whalen EA, Broeren AP, Bragg MB. Considerations for aerodynamic testing of scaled runback ice accretions Collection of Technical Papers - 44th Aiaa Aerospace Sciences Meeting. 5: 3170-3185. |
0.867 |
|
| 2006 |
Blumenthal LA, Busch GT, Broeren AP, Bragg MB. Issues in ice accretion aerodynamic simulation on a subscale model Collection of Technical Papers - 44th Aiaa Aerospace Sciences Meeting. 5: 3200-3219. |
0.864 |
|
| 2005 |
Broeren AP, Bragg MB. Effect of airfoil geometry on performance with simulated intercycle ice accretions Journal of Aircraft. 42: 121-130. DOI: 10.2514/1.4734 |
0.845 |
|
| 2005 |
Whalen E, Bragg MB. Aircraft characterization in icing using flight-test data Journal of Aircraft. 42: 792-794. DOI: 10.2514/1.11198 |
0.814 |
|
| 2005 |
Bragg MB, Broeren AP, Blumenthal LA. Iced-airfoil aerodynamics Progress in Aerospace Sciences. 41: 323-362. DOI: 10.1016/J.Paerosci.2005.07.001 |
0.821 |
|
| 2005 |
Broeren AP, LaMarre CM, Bragg MB, Lee S. Characteristics of SLD ice accretions on airfoils and their aerodynamic effects 43rd Aiaa Aerospace Sciences Meeting and Exhibit - Meeting Papers. 3027-3050. |
0.828 |
|
| 2005 |
Whalen EA, Broeren AP, Bragg MB, Lee S. Characteristics of runback ice accretions on airfoils and their aerodynamic effects 43rd Aiaa Aerospace Sciences Meeting and Exhibit - Meeting Papers. 207-220. |
0.867 |
|
| 2004 |
Broeren AP, Bragg MB, Addy HE. Effect of Intercycle Ice Accretions on Airfoil Performance Journal of Aircraft. 41: 165-174. DOI: 10.2514/1.1683 |
0.844 |
|
| 2004 |
Gurbacki HM, Bragg MB. Unsteady flowfield about an iced airfoil Aiaa Paper. 4919-4930. |
0.846 |
|
| 2004 |
Whalen EA, Melody JW, Bragg MB, Başar T. Aircraft characterization in icing using flight test data Aiaa Paper. 8421-8435. |
0.81 |
|
| 2003 |
Bragg MB, Broeren AP, Blumenthal LA. Iced-airfoil and wing aerodynamics Sae Technical Papers. DOI: 10.4271/2003-01-2098 |
0.81 |
|
| 2003 |
Lee S, Bragg MB. Investigation of factors affecting iced-airfoil aerodynamics Journal of Aircraft. 40: 499-508. DOI: 10.2514/2.3123 |
0.774 |
|
| 2003 |
Merret JM, Bragg MB. X-38 aerodynamics during rapid pitch up 21st Aiaa Applied Aerodynamics Conference. |
0.782 |
|
| 2003 |
Hossain KN, Sharma V, Bragg MB, Voulgaris PG. Envelope protection and control adaptation in icing encounters 41st Aerospace Sciences Meeting and Exhibit. |
0.596 |
|
| 2002 |
Bragg MB, Basar T, Perkins WR, Selig MS, Voulgaris PG, Melody JW, Sarter NB. Smart icing systems for aircraft icing safety 40th Aiaa Aerospace Sciences Meeting and Exhibit. DOI: 10.4271/2003-01-2100 |
0.545 |
|
| 2002 |
Gurbacki HM, Bragg MB. Unsteady aerodynamic measurements on an iced airfoil 40th Aiaa Aerospace Sciences Meeting and Exhibit. |
0.847 |
|
| 2002 |
Merret JM, Hossain KN, Bragg MB. Envelope protection and atmospheric disturbances in icing encounters 40th Aiaa Aerospace Sciences Meeting and Exhibit. |
0.86 |
|
| 2001 |
Gurbacki HM, Bragg MB. Sensing aircraft icing effects by unsteady flap hinge-moment measurement Journal of Aircraft. 38: 575-577. DOI: 10.2514/2.2801 |
0.847 |
|
| 2001 |
Broeren AP, Bragg MB. Spanwise variation in the unsteady stalling flowfields of two-dimensional airfoil models 39th Aerospace Sciences Meeting and Exhibit. DOI: 10.2514/2.1501 |
0.718 |
|
| 2001 |
Lee S, Bragg MB. The effect of ridge-ice location and the role of airfoil geometry 19th Aiaa Applied Aerodynamics Conference. |
0.606 |
|
| 2001 |
Pokhariyal D, Bragg MB, Hutchison T, Merret J. Aircraft flight dynamics with simulated ice accretion 39th Aerospace Sciences Meeting and Exhibit. |
0.558 |
|
| 2001 |
Melody JW, Pokhariyal D, Merret J, Başar T, Perkins WR, Bragg MB. Sensor integration for inflight icing characterization using neural networks 39th Aerospace Sciences Meeting and Exhibit. |
0.359 |
|
| 2000 |
Lu B, Bragg MB. Experimental investigation of airfoil drag measurement with simulated leading-edge ice using the wake survey method 18th Applied Aerodynamics Conference. |
0.533 |
|
| 2000 |
Lee S, Kim HS, Bragg MB. Investigation of factors that influence iced-airfoil aerodynamics 38th Aerospace Sciences Meeting and Exhibit. |
0.623 |
|
| 2000 |
Bragg MB, Hutchion T, Merret J, Oltman R, Pokhariyal D. Effect of ice accretion on aircraft flight dynamics 38th Aerospace Sciences Meeting and Exhibit. |
0.55 |
|
| 1999 |
Broeren AP, Bragg MB. Flowfield measurements over an airfoil during natural low-frequency oscillations near stall Aiaa Journal. 37: 130-132. DOI: 10.2514/2.678 |
0.658 |
|
| 1999 |
Saeed F, Selig MS, Bragg MB. Hybrid airfoil design procedure validation for full-scale ice accretion simulation Journal of Aircraft. 36: 769-776. DOI: 10.2514/2.2532 |
0.665 |
|
| 1999 |
Sam L, Bragg MB. Experimental investigation of simulated large-droplet ice shapes on airfoil aerodynamics Journal of Aircraft. 36: 844-850. DOI: 10.2514/2.2518 |
0.646 |
|
| 1999 |
Dunn TA, Loth E, Bragg MB. Computational investigation of simulated large-droplet ice shapes on airfoil aerodynamics Journal of Aircraft. 36: 836-843. DOI: 10.2514/2.2517 |
0.656 |
|
| 1999 |
Henze CM, Bragg MB. Turbulence intensity measurement technique for use in icing wind tunnels Journal of Aircraft. 36: 577-583. DOI: 10.2514/2.2473 |
0.577 |
|
| 1999 |
Gurbacki HM, Bragg MB. Sensing aircraft icing effects by flap hinge moment measurement 17th Applied Aerodynamics Conference. 368-378. |
0.859 |
|
| 1999 |
Kim HS, Bragg MB. Effects of leading-edge ice accretion geometry onairfoil performance 17th Applied Aerodynamics Conference. 379-391. |
0.636 |
|
| 1999 |
Lee S, Bragg MB. Effects of simulated-spanwise-ice shapes on Airfoils: Experimental investigation 37th Aerospace Sciences Meeting and Exhibit. |
0.601 |
|
| 1998 |
Saeed F, Selig MS, Bragg MB. Hybrid airfoil design method to simulate full-scale ice accretion throughout a given α range Journal of Aircraft. 35: 233-239. DOI: 10.2514/2.2289 |
0.431 |
|
| 1998 |
Jasinski WJ, Noe SC, Selig MS, Bragg MB. Wind turbine performance under icing conditions Journal of Solar Energy Engineering, Transactions of the Asme. 120: 60-65. DOI: 10.1115/1.2888048 |
0.574 |
|
| 1998 |
Broeren AP, Bragg MB. Low-frequency flowfield unsteadiness during airfoil stall and the influence of stall type 16th Aiaa Applied Aerodynamics Conference. 196-209. |
0.673 |
|
| 1998 |
Henze CM, Bragg MB, Kirn HS. Freestream turbulence measurements in icing conditions 36th Aiaa Aerospace Sciences Meeting and Exhibit. |
0.509 |
|
| 1998 |
Saeed F, Selig MS, Bragg MB, Addy HE. Experimental validation of the hybrid airfoil design procedure for full-scale ice accretion simulation 36th Aiaa Aerospace Sciences Meeting and Exhibit. |
0.538 |
|
| 1998 |
Bragg MB, Perkins WR, Sorter NB, Basar T, Voulgaris PG, Gurbacki HM, Melody JW, Mccray SA. An interdisciplinary approach to inflight aircraft icing safety 36th Aiaa Aerospace Sciences Meeting and Exhibit. |
0.853 |
|
| 1997 |
Kerho MF, Bragg MB. Airfoil boundary-layer development and transition with large leading-edge roughness Aiaa Journal. 35: 75-84. DOI: 10.2514/2.65 |
0.362 |
|
| 1997 |
Saeed F, Selig MS, Bragg MB. Design of Subscale Airfoils with Full-Scale Leading Edges for Ice Accretion Testing Journal of Aircraft. 34: 94-100. DOI: 10.2514/2.2140 |
0.345 |
|
| 1997 |
Bragg MB, Lee S, Henze CM. Heat-transfer and freestream turbulence measurements for improvement of the ice accretion physical model 35th Aerospace Sciences Meeting and Exhibit. |
0.414 |
|
| 1997 |
Saeed F, Selig MS, Bragg MB. A hybrid airfoil design method to simulate full-scale ice accretion throughout a given C1-range 35th Aerospace Sciences Meeting and Exhibit. |
0.305 |
|
| 1996 |
Bragg MB, Heinrich DC, Balow FA, Zaman KBMQ. Flow oscillation over an airfoil near stall Aiaa Journal. 34: 199-201. DOI: 10.2514/3.13045 |
0.329 |
|
| 1996 |
Bragg MB. Aicraft aerodynamic effects due to large droplet ice accretions 34th Aerospace Sciences Meeting and Exhibit. |
0.582 |
|
| 1996 |
Winkler JF, Bragg MB. Local flowfield about large distributed roughness in the initial ice accretion process 34th Aerospace Sciences Meeting and Exhibit. |
0.339 |
|
| 1996 |
Broeren AP, Bragg MB. Phase-averaged ldv flowfield measurements about an airfoil in unsteady stall 14th Applied Aerodynamics Conference. 921-931. |
0.679 |
|
| 1996 |
Bragg MB, Cummings MJ, Lee S, Henze CM. Boundary-layer and heat-transfer measurements on an airfoil with simulated ice roughness 34th Aerospace Sciences Meeting and Exhibit. |
0.354 |
|
| 1995 |
Bragg MB, Khodadoust A. Study of the droplet spray characteristics of a subsonic wind tunnel Journal of Aircraft. 32: 199-204. DOI: 10.2514/3.46701 |
0.351 |
|
| 1995 |
Khodadoust A, Bragg MB. Aerodynamics of a finite wing with simulated ice Journal of Aircraft. 32: 137-144. DOI: 10.2514/3.46694 |
0.505 |
|
| 1994 |
Bragg MB, Heinrich DC, Valarezo WO, McGhee RJ. Effect of underwing frost on a transport aircraft airfoil at flight Reynolds number Journal of Aircraft. 31: 1372-1379. DOI: 10.2514/3.46661 |
0.438 |
|
| 1994 |
Bragg MB, Wells SL. Effect of wind-tunnel walls on airfoil droplet impingement Journal of Aircraft. 31: 175-180. DOI: 10.2514/3.46471 |
0.38 |
|
| 1994 |
Kerho MF, Bragg MB. Neutrally buoyant bubbles used as flow tracers in air Experiments in Fluids. 16: 393-400. DOI: 10.1007/Bf00202064 |
0.335 |
|
| 1993 |
Soltani MR, Bragg MB. Early vortex burst on a delta wing in pitch Aiaa Journal. 31: 2283-2289. DOI: 10.2514/3.11926 |
0.347 |
|
| 1992 |
Bragg MB, Mohler SH. Predicting droplet impingement on yawed wings Journal of Aircraft. 29: 964-966. DOI: 10.2514/3.46270 |
0.321 |
|
| 1992 |
Bragg MB, Khodadoust A, Spring SA. Measurements in a leading-edge separation bubble due to a simulated airfoil ice accretion Aiaa Journal. 30: 1462-1467. DOI: 10.2514/3.11087 |
0.549 |
|
| 1990 |
Soltani MR, Bragg MB, Brandon JM. Measurements on an oscillating 70-deg delta wing in subsonic flow Journal of Aircraft. 27: 211-217. DOI: 10.2514/3.45921 |
0.377 |
|
| 1988 |
Bragg MB. Experimental aerodynamic characteristics of an NACA 0012 airfoil with simulated glaze ice Journal of Aircraft. 25: 849-854. DOI: 10.2514/3.45669 |
0.702 |
|
| 1987 |
Bragg MB, Gregorek GM. EXPERIMENTAL STUDY OF AIRFOIL PERFORMANCE WITH VORTEX GENERATORS Journal of Aircraft. 24: 305-309. DOI: 10.2514/3.45445 |
0.385 |
|
| 1987 |
Coirier WJ, Bragg MB. COMPUTATIONAL METHOD FOR SCREENED TWO-DIMENSIONAL WIND TUNNEL INLETS Journal of Aircraft. 24: 281-283. DOI: 10.2514/3.45438 |
0.332 |
|
| 1986 |
Bragg MB, Gregorek GM, Lee JD. Airfoil aerodynamics in icing conditions Journal of Aircraft. 23: 76-81. DOI: 10.2514/3.45269 |
0.663 |
|
| 1986 |
Bragg MB, Coirier WJ. AERODYNAMIC MEASUREMENTS OF AN AIRFOIL WITH SIMULATED GLAZE ICE Aiaa Paper. |
0.613 |
|
| 1985 |
Bragg MB. PREDICTING RIME ICE ACCRETION ON AIRFOILS Aiaa Journal. 23: 381-387. DOI: 10.2514/3.8924 |
0.584 |
|
| 1985 |
Bragg MB, Coirier WJ. DETAILED MEASUREMENTS OF THE FLOWFIELD IN THE VICINITY OF AN AIRFOIL WITH GLAZE ICE Aiaa Paper. |
0.596 |
|
| 1984 |
Bragg MB. Effect of geometry on airfoil icing characteristics Journal of Aircraft. 21: 505-511. DOI: 10.2514/3.45000 |
0.445 |
|
| 1984 |
Bragg MB, Gregorek GM, Lee JD. EXPERIMENTAL AND ANALYTICAL INVESTIGATIONS INTO AIRFOIL ICING Congress of the International Council of the Aeronautical Sciences. 2: 1127-1138. |
0.588 |
|
| 1983 |
Bragg MB, Gregorek GM. Predicting aircraft performance degradation due to ice accretion Sae Technical Papers. DOI: 10.4271/830742 |
0.549 |
|
| 1982 |
Bragg MB. A similarity analysis of the droplet trajectory equation Aiaa Journal. 20: 1681-1686. DOI: 10.2514/3.8004 |
0.319 |
|
| 1981 |
Bragg MB, Gregorek GM, Shaw RJ. ANALYTICAL APPROACH TO AIRFOIL ICING Aiaa Paper. |
0.572 |
|
| Show low-probability matches. |
