SAE Technical Paper Series 2007
DOI: 10.4271/2007-01-3311
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Appendix D - An Interim Icing Envelope

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Cited by 17 publications
(14 citation statements)
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“…Motivated by the 1990s commuter jet engine power loss problem, Lawson et al (1998) reanalyzed more limited in situ measurements collected within anvils over Montana during the Cooperative-Convective-Precipitation-Experiment (CCOPE) (Knight, 1982) and near the Tiwi Islands during the Central Equatorial Pacific Experiment (CEPEX) (Heymsfield and McFarquhar, 1996;McFarquhar and Heymsfield, 1996). Since no direct measurements of IWC were obtained during these campaigns, it was calculated from the most suitable data available.…”
Section: Microphysical Conditionsmentioning
confidence: 99%
“…Motivated by the 1990s commuter jet engine power loss problem, Lawson et al (1998) reanalyzed more limited in situ measurements collected within anvils over Montana during the Cooperative-Convective-Precipitation-Experiment (CCOPE) (Knight, 1982) and near the Tiwi Islands during the Central Equatorial Pacific Experiment (CEPEX) (Heymsfield and McFarquhar, 1996;McFarquhar and Heymsfield, 1996). Since no direct measurements of IWC were obtained during these campaigns, it was calculated from the most suitable data available.…”
Section: Microphysical Conditionsmentioning
confidence: 99%
“…An early Royal Aircraft Establishment report by McNaughton (1959), which has been used for years to provide some guidelines to aviation on ice water content, describes measurements made in convective clouds near Entebbe, Singapore and Darwin with total water contents (probably mostly ice) exceeding 5 g m −3 . Mazzawy and Strapp (2007) summarize these and other measurements in order to come up with "Appendix D -An Interim Icing Envelope" which defines a mixed phase/glaciated icing environment to be used by the aviation industry in certifying engines for operations in these conditions.…”
Section: Introductionmentioning
confidence: 99%
“…The sampling strategy was consistent with 2015 in terms of the sampling altitudes (-50°C±5°C, -40°C±5°C, -30°C±5°C and -10°C±5°C), but with an added interest to fly also at -25°C±5°C levels when mission rules allowed. Based on adiabatic estimates of maximum condensed water that are the basis of the Appendix D TWC envelope [1],and numerical simulation results by Protor, et al [22], there was reason to believe that TWC values might maximize in the -20° to -30°C temperature interval. This flight level was not identified as a priority by the EHWG, and was not a focus for the HAIC-HIWC and first HIWC RADAR campaigns.…”
Section: Sampling Strategiesmentioning
confidence: 99%
“…In 2003, the FAA chartered an Aviation Rulemaking Advisory Committee (ARAC) called the Engine Harmonization Working Group (EHWG) to evaluate the effects of supercooled large drop (SLD) and mixed phase/glaciated conditions on commercial transport power plants [1]. The EHWG found that most weather-related engine powerloss events on commercial aircraft had occurred in or near deep convective storms.…”
Section: Introductionmentioning
confidence: 99%