LEADER 03798nam 2200613 450 001 9910438322303321 005 20221206101420.0 010 $a0-7680-8713-9 010 $a0-7680-8189-0 010 $a1-5231-0224-1 024 7 $a10.4271/PT-163 035 $a(CKB)3710000000729216 035 $a(SSID)ssj0001654321 035 $a(PQKBManifestationID)16434061 035 $a(PQKBTitleCode)TC0001654321 035 $a(PQKBWorkID)14983327 035 $a(PQKB)11608790 035 $a(MiAaPQ)EBC5341862 035 $a(CaBNVSL)mat08504291 035 $a(IDAMS)0b00006488764975 035 $a(IEEE)8504291 035 $a(EXLCZ)993710000000729216 100 $a20181229d2015 uy 101 0 $aeng 135 $aurcnu|||||||| 181 $ctxt 182 $cc 183 $acr 200 10$aIce accretion and icing technology /$fRobert J. Flemming 210 1$aWarrendale, Pa. (400 Commonwealth Dr., Wallendale PA USA) :$cSociety of Automotive Engineers,$d2015. 210 2$a[Piscataqay, New Jersey] :$cIEEE Xplore,$d[2015] 215 $a1 online resource (xii, 107 pages) $cillustrations 225 1 $aSociety of Automotive Engineers. Electronic publications 300 $aMinimal Level Cataloging Plus.$5DLC 311 $a0-7680-8120-3 320 $aIncludes bibliographical references. 327 $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. 330 $aThis title addresses, among other topics, the measurement techniques and the drop physics that apply to icing, certification for flight through ice crystal clouds and in supercooled large drops, improvements in predictive techniques, scaling methods, test facilities and techniques, and rotorcraft icing. The effects of inflight atmospheric icing can be devastating to aircraft. Universities and industry have been hard at work to respond to the challenge of maintaining flight safety in all weather conditions. ...Proposed changes in the regulations for operation in icing conditions are sure to keep this type of research and development at its highest level. This is especially true for the effects of ice crystals in the atmosphere, and for the threat associated with supercooled large drop (SLD) icing. 410 0$aSociety of Automotive Engineers. Electronic publications 606 $aAirplanes$xIce prevention 606 $aAeronautics$xSafety meaures 606 $aAirplanes$xClimatic factors 615 0$aAirplanes$xIce prevention. 615 0$aAeronautics$xSafety meaures. 615 0$aAirplanes$xClimatic factors. 676 $a629.13432 700 $aFlemming$b Robert J.$01249649 801 0$bCaBNVSL 801 1$bCaBNVSL 801 2$bCaBNVSL 906 $aBOOK 912 $a9910438322303321 996 $aIce accretion and icing technology$92895844 997 $aUNINA