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DATA/ALK3.D/data.ms �2���������������������������������������������������������������������������������������������������������������������������������������������������������������������������������17 SEP 104 10:28 ���������������������������������������������������������������÷ě���z�������������ű� )q��sö�5÷l��4�����������������������������������������������������������������������������������������������������������������������������������������������������������������������������...

MINEX2-unsorted-pruned-CC/README The MINEX II Sample Data for Matching is comprised of 42 templates in ISO compact card format. These templates were created from ANSI 378 templates, and are not sorted. The templates are used to validate correct operation of the submitted SDK on the NIST test platform prior to the start of testing. The templates are representative of the FORMAT of the actual test data only. They are not intended to be representative of the test data in terms of number of minutiae or other characteristics. Participants shall compute the results of matching 100 pairs of templates from this set with their SDK, and return the scores to the Test Liaison (by email). If more than one SDK will be submitted, the process shown below shall be repeated for each additional SDK. STEPS ===== 1) Compute match scores for all 100 pairs of templates listed in the file "sd24pairs.lst". The format of this file is: [Probe Template Filename] [Gallery Template Filename] ------------------------------------------------------------------- **NOTE: Each score shall be produced by matching the Probe Template against the Gallery Template (in that order). ------------------------------------------------------------------- 2) Return the results to NIST (minexII@nist.gov) as a single ASCII text file (for each SDK submit...

MINEX2-YX_descending-pruned-CC/README The MINEX II Sample Data for Matching is comprised of 42 templates in ISO compact card format. These templates were created from ANSI 378 templates sorted Y-X descending. The templates are used to validate correct operation of the submitted SDK on the NIST test platform prior to the start of testing. The templates are representative of the FORMAT of the actual test data only. They are not intended to be representative of the test data in terms of number of minutiae or other characteristics. Participants shall compute the results of matching 100 pairs of templates from this set with their SDK, and return the scores to the Test Liaison (by email). If more than one SDK will be submitted, the process shown below shall be repeated for each additional SDK. STEPS ===== 1) Compute match scores for all 100 pairs of templates listed in the file "sd24pairs.lst". The format of this file is: [Probe Template Filename] [Gallery Template Filename] ------------------------------------------------------------------- **NOTE: Each score shall be produced by matching the Probe Template against the Gallery Template (in that order). ------------------------------------------------------------------- 2) Return the results to NIST (minexII@nist.gov) as a single ASCII text file (for each SDK...

IKA®RV 10 basic IKA®RV 10 digital 042009 Betriebsanleitung DE 5 Operating instructions EN 17 Mode d’emploi FR 29 Instrucciones de manejo ES 41 36 785 00 Reg.-No. 4343-01 3678500_RV10bd_032009_4sprachig_ue:Layout 1 22.07.2009 17:30 Uhr Seite 1 3042009 EG-KONFORMITÄTSERKLÄRUNG DE Wir erklären in alleiniger Verantwortung, dass dieses Produkt den Bestimmungen der Richtlinien 2006/95/EG, 98/37/EG und 2004/108/EG entspricht und mit den folgenden Normen und norminativen Dokumenten übereinstimmt: DIN EN IEC 61010-1, -2-051; DIN EN ISO 12100-1, -2; EN 60204-1 und DIN EN IEC 61326-1. CE-DECLARATION OF CONFORMITY EN We declare under our sole responsibility that this product corresponds to the regulations 2006/95/EC, 98/37/EC and 2004/108/EC and conforms with the standards or standardized documents DIN EN IEC 61010-1, -2-051; DIN EN ISO 12100-1, -2; EN 60204-1 and DIN EN IEC 61326-1. DÉCLARATION DE CONFORMITÉ CE FR Nous déclarons sous notre propre responsabilité que ce produit est conforme aux réglementations 2006/95/CE, 98/37/CE et 2004/108/CE et en conformité avec les normes ou documents normalisés suivant DIN EN IEC 61010-1, -2-051; DIN EN ISO 12100-1, -2; EN 60204-1 et DIN EN IEC 61326-1. DECLARACION DE CONFORMIDAD DE CE ES Declaramos por nuestra responsabilidad propia que este producto corresponde a las directrices 2006/...

PHYSICAL AND CHEMICAL ASPECTS OF CUP-BURNER FLAME EXTINGUISHMENT Fumiaki Takahashi National Center for Space Exploration Research on Fluids and Combustion NASA Glenn Research Center, Cleveland, OH 44135 USA Tel: 216-433-3778; Fax: 216-433-8050; Fumiaki.Takahashi@grc.nasa.gov Gregory T. Linteris Fire Research Division, National Institute of Standards and Technology Gaithersburg, MD 20899 USA Tel: 301-975-2283; Fax: 301-975-4052; linteris@nist.gov Viswanath R. Katta Innovative Scientific Solutions, Inc., Dayton, OH, 45440 USA Tel: 937-255-8781; Fax: 937-656-4110; vrkatta@erinet.com * ABSTRACT Extinguishing limits of laminar methane-air co-flow diffusion flames in a cup-burner apparatus in normal earth gravity have been determined experimentally and computationally. A gaseous fire-extinguishing agent (Ar, He, N2, CO2, CF3H, CF3Br, or Br2) was added gradually into the coflowing oxidizer until the flame extinguished. The extinguishment of cup-burner flames, which resemble real fires, occurred via a blowoff process (in which the flame base oscillated before drifted downstream eventually) rather than the global extinction typical of counterflow diffusion flames. Unsteady numerical simulations with detailed chemistry revealed that the peak reactivity spot (i.e., reaction kernel), formed at the flame attach...

minex2_sd4templategen/a001_03p.RAW minex2_sd4templategen/a001_04p.RAW minex2_sd4templategen/a001_05p.RAW minex2_sd4templategen/a001_06p.RAW minex2_sd4templategen/a001_07p.RAW minex2_sd4templategen/a004_05p.RAW minex2_sd4templategen/a999_01p.RAW minex2_sd4templategen/b001_04p.RAW minex2_sd4templategen/b001_06p.RAW minex2_sd4templategen/b001_08p.RAW �������﻾����﷿ﻻ��ﳿ粒ﷺ���﻾﷾﫼粒ﳹ�����﫽笠ﯻﳻ﻽﷾���﫸ﻼ���ﳿ﫹ﳼ﻽ﳿﷹ﷿ﳻ��������ﯻ﷽﻽���������﷿ﯹ��ﳽﳼﳼ﷼���﷿﫺ﻼ�﷿ﯻﻻ���ﯺ﷼��﻾��ﳼ�����﷾﷽ﳽ���ﯻﳻ﻽﻾��﷿﫺ﷻ�ﳽﯻ������﻾﻾﻾﻾﻾﻾﻾�����������﷽﻽﻾﷽�����������������ﳾﯺ﫼﫹ﷻ������ﯽﷹ��﷿炙ﯹ��﷿���﻾�ﳿ狀﫹��﷿﫹炙ﳸ�������������ﳻ��﻽������﷾﻽��﷾��������﷽��������﻾�����﻽�﻾﻾��﷾���﻾��﻾��﻾���﻾﻾﻾����������﷽﷽ﳾﯻﻼ�...

NIST Special Publication 1069 Richard G. Gann, Editor Building and Fire Research Laboratory The Final Report of the Next Generation Fire Suppression Technology Program Advanced Technology for Fire Suppression in Aircraft U.S. Department of Commerce Carlos M. Gutierrez, Secretary Technology Administration Robert C. Cresanti, Under Secretary for Technology National Institute of Standards and Technology William A. Jeffrey, Director June 2007 Page intentionally left blank Certain commercial entities, equipment, or materials are identified in this document in order to describe an experimental procedure or concept adequately. Such identification is not intended to imply recommendation or endorsement by the National Institute of Standards and Technology or the Strategic Environmental Research and Development Program, nor is it intended to imply that the entities, materials, or equipment are necessarily the best available for the purpose. The policy of NIST is to use metric units of measurement in all its publications, and to provide statements of uncertainty for all original measurements. In this document, however, data from organizations outside NIST are shown. These data may include measurements in non- metric units or measurements without uncertainty statements. National Institute of St...

Dynamic Mechanical Analysis/20150620_analyzed.xlsx Data Specimen ID 20150620 1Visual beginning temperature of glass transition region, (°C) 50 Material ID SG300-ARL 1Visual ending temperature of glass transition region, (°C) 100 Row of beginning temperature of glass transition region 741 Load vs Extension Row of ending temperature of glass transition region 1242 Load vs Shifted Extension 2Frequency (hz) Row of glass transition temperature from Loss Modulus 949 Document Doc Description Target Indexed Display as record 2Heating rate (°C/min) 2Glass transition temperature (°C), from Loss Modulus 70 !FILENAME _blank TRUE FALSE Loss modulus @ Tg 125 Row of glass transition temperature from Tan Delta 242 Analysis Date 7/15/15 2Glass transition temperature (°C), from Tan Delta 1 Temperatures 25 °C Tan delta @ Tg 0.347 -51 °C Row of temperature = 25°C 491 71 °C Valid Test TRUE 3Storage modulus @ 25°C 1503 Use in Summary TRUE 3Loss modulus @ 25°C 84 3Tan delta @ 25°C 0.301 4Row of temperature = -51°C ERROR:#N/A Projected Start 31 Storage modulus @ -51°C ERROR:#N/A Start Row 31 Loss modulus @ -51°C ERROR:#N/A End Row 1818 Tan delta @ -51°C ERROR:#N/A Last Row 1818 5Row of temperature = 71°C 943 Storage modulus @ 71°C 55...

Dynamic mechanical analysis/Hysol 9309 1.001 CLOSED VERSION 2.0 Language English Run 1 RunSerial 2649 Instrument DMA Q800 V20.16 Build 35 Module DMA Multi-Frequency - Strain Operator MS File \\Ta-workstation\ta\Data\DMA\Silton\Hysol 9309 1.001 ProcName InstSerial 0800-0958 Clamp Single Cantilever Sample Hysol 9309-1 Geometry Rectangular (Length, Width, Thickness) GeomFactor 31.4784 1/mm 0.0211 1/mm 0.6648 1/mm² Size 17.3300 12.4133 2.5100 mm SampParams 0.3500 Method Comment Xcomment Air Bearing Gas: Air Text FreqTab 1.00, Multiplex None InstCalDate Electronics: 2015-05-08 08:40:59 0.0001 InstCalDate Force: 2015-05-08 09:19:34 0.0096 Enabled InstCalDate Dynamic: 2015-05-08 13:07:48 0.0156 Enabled InstCalDate Clamp Date: 2015-05-28 13:42:24 InstCalDate Clamp Mass: 29.2 gm InstCalDate Clamp Offset: 0.00 mm InstCalDate Clamp Compliance: 0.721 um/N TempCal 0 pts Settings OscStrain 0.0200 MinOscF 0.0000 StabCyc 4 AvgCyc 3 StoreStable AutoZero LengthFixed Controls Gas 1 Event Off Sampling 1.0 AutoAnalysis Off MacroFile Nsig 17 Sig1 Time (min) Sig2 Temperature (°C) Sig3 Storage Modulus (MPa) Sig4 Loss Modulus (MPa) Sig5 Stress (MPa) Sig6 Tan Delta Sig7 Frequency (Hz) Sig8 Drive Force (N) Sig9 Amplitude (µm) Sig10 Strain (%) Sig11 Displacement (µm...