MARC Record from marc_columbia

LEADER: 04353cam a2200613 i 4500
001 12174224
005 20221203224053.0
006 m eo d
007 cr bn||||m|||a
008 150902s2015 paua ob 000 0 eng d
035 $a(OCoLC)ocn919637213
035 $a(NNC)12174224
040 $aCaBNVSL$beng$erda$epn$cJ2I$dJ2I$dOCLCO$dKNOVL$dSTF$dCUV$dESU$dOCLCF$dCEF$dRRP$dUK7LJ$dIEEEE$dPASAE$dOCLCO$dUTBLW$dOCLCQ$dUPM
020 $a9781523102242$q(electronic bk.)
020 $a1523102241$q(electronic bk.)
020 $z9780768081893
020 $z0768081890
020 $z9780768081206$q(print)
020 $z9780768081916
020 $z0768081912
020 $z9780768081909
020 $z0768081904
024 7 $a10.4271/PT-163$2doi
035 $a(OCoLC)919637213
050 4 $aTL557.I3$bF54 2015eb
082 04 $a629.1325214$223
049 $aZCUA
100 1 $aFlemming, Robert J.,$eauthor.
245 10 $aIce accretion and icing technology /$cRobert J. Flemming.
264 1 $aWarrendale, Pa. (400 Commonwealth Dr., Warrendale PA USA) :$bSociety of Automotive Engineers,$c[2015]
300 $a1 online resource (xii, 107 pages) :$billustrations (some color)
336 $atext$btxt$2rdacontent
337 $acomputer$bc$2rdamedia
338 $aonline resource$bcr$2rdacarrier
490 1 $aSociety of Automotive Engineers. Electronic publications
500 $aTitle from PDF title page (SAE Web site, 08/25/2015)
504 $aIncludes bibliographical references.
505 0 $aIntroduction -- Effect of stagnation flow on an impacting water droplet on a superhydrophobic surface (2013-01-2174) -- Icing process of supercooled-water droplet moving on a surface by using luminescent temperature-imaging technique (2013-01-2210) -- Considerations on the use of hydrophobic, superhydrophobic or icephobic coatings as a part of the aircraft ice protection system (2013-01-2108) -- Evaluation of icing scaling on swept NACA 0012 airfoil models (2011-38-0081) -- New SLD icing capabilities at DGA aero-engine testing (2011-38-0086) -- S-76D tail rotor ice impact test (2011-38-0101) -- Numerical correlation between meteorological parameters and aerodynamic performance degradation of iced airfoils (2013-01-2137) -- Calculation of ice shapes on oscillating airfoils (2011-38-0015) -- Oscillating airfoil icing tests in the NASA Glenn Research Center Icing Research Tunnel (2011-38-0016) -- In-flight icing of UAVs -- The influence of Reynolds Number on the ice accretion process (2011-01-2572) -- About the editor.
520 $aThis title addresses, among other topics, the measurement techniques and the drop physics that apply to icing, certification for flight through ice crystal clouds and in supercooled large drops, improvements in predictive techniques, scaling methods, test facilities and techniques, and rotorcraft icing. The effects of inflight atmospheric icing can be devastating to aircraft. Universities and industry have been hard at work to respond to the challenge of maintaining flight safety in all weather conditions. ... Proposed changes in the regulations for operation in icing conditions are sure to keep this type of research and development at its highest level. This is especially true for the effects of ice crystals in the atmosphere, and for the threat associated with supercooled large drop (SLD) icing.
650 0 $aAeronautics$xSafety meaures.
650 0 $aAirplanes$xIce prevention.
650 0 $aAirplanes$xClimatic factors.
650 6 $aAvions$xGivrage$xPrévention.
650 7 $aTECHNOLOGY & ENGINEERING$xAeronautics & Astronautics.$2bisacsh
650 7 $aSCIENCE$xEarth Sciences$xMeteorology & Climatology.$2bisacsh
650 7 $aAirplanes$xClimatic factors.$2fast$0(OCoLC)fst00803077
650 7 $aAirplanes$xIce prevention.$2fast$0(OCoLC)fst00803239
655 0 $aElectronic books.
655 4 $aElectronic books.
710 2 $aSociety of Automotive Engineers,$epublisher.
776 08 $iPrint version:$aFlemming, Robert J.$tIce accretion and icing technology.$dWarrendale, PA : SAE International, [2015]$z0768081203$w(OCoLC)919015276
810 2 $aSociety of Automotive Engineers.$tElectronic publications.
856 40 $uhttp://www.columbia.edu/cgi-bin/cul/resolve?clio12174224$zACADEMIC - Aerospace & Radar Technology
852 8 $blweb$hEBOOKS