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"After may refer to: Literature *After (Elgar), an 1895 poem by Philip Bourke Marston set to music by Edward Elgar *After (Prose novel), a 2003 novel by Francine Prose *After (Todd novel), a novel by Anna Todd *After... (visual novel), a 2003 eroge visual novel *After (book), a 2005 book by Canadian writer Francis Chalifour *After (series), a 2013 fan fiction book by Wattpad writer Anna Todd Music *After (Ihsahn album), 2010 * After (Lady Lamb album), 2015 *After (Sammi Cheng album), 1995 *"After" (song), a 2011 song by Moby *(after), a 2018 live album by Mount Eerie *"After", a 2014 song by Amy Lee featuring Dave Eggar from the album Aftermath TV and film * After... (film), a 2006 supernatural thriller * After (2012 film), a 2012 sci-fi thriller film written and directed by Ryan Smith * After, a 2012 film starring Julie Gayet * After (2019 film), a 2019 American film, based on the 2013 book * "After" (The Walking Dead), an episode of the television series The Walking Dead Other *After, in naval terminology, an adjective for distinguishing parts of a ship nearer the aft See also Arter, eye dialect spelling of "after" * "Afterward", a 1910 short story by Edith Wharton * Later (disambiguation) "
"Marcel Khalife (; b. June 10, 1950, Amsheet, Mount Lebanon Governorate, Lebanon) is a Lebanese composer, singer, and oud player. Biography May Day celebration in Beirut In 1983, Paredon Records, now Smithsonian Folkways, released Promises of the Storm, a small collection of protest songs and political ballads.Khalife at Smithsonian Folkways =Tunisia= In July 2009, Khalife returned to Tunisia to perform on the stage of the Roman amphitheatre to a full house, as part of the 45th International Festival of Carthage. Speaking to the audience, Khalife opened the concert by stating:Committed Marcel Khalifa Re-visits Fans in Tunisia by Iman Zayat, Alarab Online, July 29, 2009 Khalife later dedicated a song to the "revolutionary leader Che Guevara". =Ana Yousef, ya Abi case= Three times (1996, 1999 and 2003), he faced criminal prosecution for his song I am Joseph, O Father, written by the Palestinian poet Mahmoud Darwish.I am Yusuf, oh my father Personal life His eldest son, Juilliard School graduate Rami Khalife, is a pianist and composer. In October 2011, the Qatar Philharmonic Orchestra, under the conductorship of James Gaffigan, premiered Khalife's 'Chaos', for orchestra and piano, with Khalife at the helm as a soloist. In February 2013, Rami Khalife's Arab Spring-inspired 'Requiem' was premiered, within the same program as Marcel Khalife's suite "Oriental". WorksBooks= In 1982, the composer wrote a six-part Anthology of Studying the Oud. =Performances= *2005.11.14: Lincoln Theatre (Washington, D.C.) USA *2004.01.12: Kennedy Center Washington DC USA *2008.10.10: De Roma Borgerhout, Antwerp, Belgium *2011.03.13: Al-Bustan Concert Series, Philadelphia, PA, USA *2014.11.15: Al-Bustan Concert Series, Philadelphia, PA, USA *2016.12.18: Day for Night Festival, Houston, TX, USAhttp://www.dayfornight.io/schedule/ *2018.05.25 Institut des cultures arabes et méditerranéennes,Geneva, Switzerland =Films= Marcel Khalife has composed soundtracks for films, documentaries and fictions, produced by Maroun Baghdadi, Oussama Mohammed, Sophi Sayhf Eddin and Samir Zikra. His music is also featured in the documentary Occupied Minds produced by Jamal Dajani and David Michaelis. His music featured in the documentary film Sons of Eilaboun by Hisham Zreiq.The Sons of Eilaboun – official website =Talks= Marcel Khalife gave a talk on March 12, 2013, at the American University of Sharjah about his latest CD, The Fall of the Moon, and his longing towards the late Mahmoud Darwish. He also spoke about prospects of publishing his autobiography in two volumes. Discography Below the discography of Marcel Khalife. =Studio albums= * Storm Promises (1976) * At the Border (1980) * Ahmad Al Arabi (1984) * Dreamy Sunrise (1985) * Ode to a Homeland (1990) * Arabic Coffeepot (1995) * Voyageur (1998) * Jadal (2002) * The Bridge (2002) * Summer Night's Dream (2003) * Promises of the Storm (2003) * Caress (2004) * Peace Be with You (2006) * Taqasim (2006) * Sharq (2007) =Singles= * Mounadiloun (Strugglers) * Oummi (Mother) =Live albums= * Dance (1995) * Marcel Khalife: Magic Carpet (1998) * Concerto Al Andalus (2002) ReferencesEnglish= * Marcel Khalife Discusses the New and the Old in Arabic Music in a Leading Literary Supplement: The Rationalization of Arabic Music, Translated and edited by Elie Chalala, Al Jadid magazine, Vol. 1, no. 1 (November 1995) * Trial of famous Lebanese singer to begin: Marcel Khalifa Faces Three Years in Prison * Music as a Mission: Marcel Khalife strums the heartbeat of the Arab world * Lebanese singer banned in Tunisia * Biography * Interview with Marcel Khalife =French= * Marcel Khalifé: Voyageur..., Pierre Dupouey, mardi 10 février 2004 * Marcel Khalife poursuivi en justice: entre versets et sonnets, Taïeb Chadi * Visages, Dalia Chams * Biographie External links * * UNESCO artist for peace * Rawafed interview/Marcel Khalife Category:1950 births Category:Living people Category:Lebanese musicians Category:Lebanese oud players Category:Lebanese songwriters Category:Lebanese male singers Category:People from Amsheet Category:Lebanese Maronites "
"The Junkers Jumo 213 was a World War II-era V-12 liquid-cooled aircraft engine, a development of Junkers Motoren's earlier design, the Jumo 211. The design added two features, a pressurized cooling system that required considerably less cooling fluid that allowed the engine to be built smaller and lighter, and a number of improvements that allowed it to run at higher RPM. These changes boosted power by over 500 hp and made the 213 one of the most sought-after Axis engine designs in the late-war era. Design and development When the Jumo 211 entered production in the late 1930s it used an unpressurized liquid cooling system based on an "open cycle". Water was pumped through the engine to keep it cool, but the system operated at atmospheric pressure, or only slightly higher. Since the boiling point of water decreases with altitude (pressure) this meant that the temperature of the cooling water had to be kept quite low to avoid boiling at high altitudes, which in turn meant that the water removed less heat from the engine before flowing into the radiator to cool it. By contrast, the 1940 Daimler-Benz DB 601E used a pressurized coolant system that ran at the same pressure regardless of altitude, raising the boiling point to about 110 °C. This allowed it to use considerably less water for the same cooling effect, which remained the same at all altitudes. Although otherwise similar to the Jumo 210 in most respects, the 601 was smaller and lighter than the 211, and could be run at higher power settings at higher altitudes, making it popular in fighter designs. The 211 was relegated to "secondary" roles in bombers and transports. The Junkers Motorenwerke firm was not happy with this state of affairs, and started its own efforts to produce a pressurized cooling system as early as 1938. Experiments on the 211 proved so successful that it became clear that not only could the engine be built smaller and lighter (by reducing the water requirement),Christopher, p. 78 but could be run at higher power settings without overheating. Additional changes to strengthen the crankshaft and add a fully shrouded supercharger for increased boost resulted in the Jumo 211F model, which delivered 1,340 PS (1,322 hp, 986 kW) at 2,600 RPM, up from 1000 PS at 2,200 RPM in the first version 211A. Jumo 213 fuel injector system components in the Technikmuseum Speyer But this was only the beginning. After redesigning the engine block to a smaller external size to suit the increased cooling power – while keeping the same 150 mm x 165 mm bore/stroke figures, maintaining the 35 litre displacement of the Jumo 211 series – and then further increasing boost settings on the supercharger, the resulting 213A model was able to deliver 1,750 PS (metric hp) at 3,250 RPM. This made it considerably more powerful than the corresponding DB 601E which provided 1,350 PS, and about the same power as the much larger DB 603 of 44.52 litre displacement. Junkers decided to go after the 603's market, and placed the 213's mounting points and fluid connections in the same locations as the 603, allowing it to be "dropped in" as a replacement, with the exception of the Jumo's standard starboard-side supercharger intake (Daimler-Benz inverted V12 engines always had the supercharger intakes on the port side). The 213A (the main production series, with single-stage two-speed supercharging)Christopher, p. 79 first ran in 1940, but experienced lengthy delays before finally being declared "production quality" in 1943. Production was extremely slow to ramp up, in order to avoid delays in the existing Jumo 211 production. By the time the engines were available in any sort of number in 1944, Allied bombing repeatedly destroyed the production lines. Production of the A model was limited to about 400–500 a month for most of 1944/45. A range of advanced versions were also developed during the lengthy teething period. The 213B was designed to run on 100 octane "C3" fuel, allowing the boost pressure to be increased and the take-off power improved to 2,000 PS. The 213C was essentially an A model with re-arranged secondary equipment (supercharger, oil pump, etc.) to allow a Motorkanone cannon to fire through the propeller shaft. The 213D added a new three-speed supercharger for smoother power curves and improved altitude performance, but it was not produced. Junkers Jumo 213E-1 at Flugmuseum Aviaticum in Wiener Neustadt, Austria The next major production versions were the 213E and the similar 213F. These engines were equipped with a new two-speed, two-stage supercharger that dramatically improved altitude performance. The only difference between the two models was that the E included an intercooler for additional high-altitude performance, while the F model lacked this and was optimized for slightly lower altitudes. The E and F models were in high demand for many late-war aircraft, including the Junkers Ju 188, Junkers Ju 388, the Langnasen-Dora models of the Focke-Wulf Fw 190D and the Focke-Wulf Ta 152H. All of these aircraft used annular radiators characteristic of the earlier Jumo 211 engine installations on twin-engined aircraft, often standardized as Kraftei (power-egg), completely unitized power plant "modules" for any twin or multi-engined aircraft, much as the Jumo 211 had evolved for earlier aircraft designs – but with the annular radiators noticeably reconfigured for better cooling of the more powerful Jumo 213 engine. A further substantial upgrade was projected as the 213J, which replaced the earlier model's three valves with a new four-valve-per-cylinder design for increased volumetric efficiency. It was also to have had a two- stage three-speed supercharger, producing at 3700 rpm for take-off. It would have weighed . There was no time to work this change into the production line before the war ended. Other experimental models included the 213S for low- altitude use, and the turbocharged 213T. Further development of the Jumo 213 was carried out at Arsenal de l'Aéronautique in France after the Second World War. Variants A Jumo 213-powered Ju 188, with reconfigured annular radiators ;213A: First version, 1,750 PS (2,100 PS with MW50 boost) take-off power, major production version. ;213B: Project, a 213A with C3 fuel (100 octane) and up to 2,000 PS take-off power. ;213C: As 213A but equipped for mounting of a cannon firing through the propeller axis (Motorkanone), limited production. ;213D: 213C with a new three-speed supercharger, did not enter production. ;213E: High altitude version of 213A, equipped with a three-speed two-stage intercooled supercharger and delivering 1,750 PS take-off power (2,050 PS with MW 50 boost). ;213F:Similar to the 213E, but without the intercooler. ;213J:Project, redesigned with four valves per-cylinder and a two-stage three-speed supercharger, delivering 2,380 PS at takeoff. ;J13T:Proposed turbocharged variant. ;Arsenal 12H:Post-war development of the Junkers Jumo 213 which had been in production for the Germans at the Arsenal de l'Aéronautique factories. ;Arsenal 12H-Tandem:2x 12H engines in tandem driving co-axial propellers. ;Arsenal 12K:Further development of the 12H. ;Arsenal 24H:A 24-cylinder H-24 engine utilizing 12H cylinder blocks, crankshafts and pistons mounted on a new crankcase driving a single propeller. ;Arsenal 24H-Tandem:2x 24H engines in tandem driving co-axial propellers. ;SFECMAS 12H: The Arsenal 12H after SFECMAS absorbed Arsenal. ;SFECMAS 12K: The Arsenal 12K after SFECMAS absorbed Arsenal. Applications * Heinkel He 111H-22 * Junkers Ju 88 * Junkers Ju 188 * Junkers Ju 388 * Focke-Wulf Fw 190D * Focke-Wulf Ta 152 * Focke-Wulf Ta 154 * Messerschmitt Me 209-II * Nord Noroit * SNCASO SO.8000 Narval Specifications (Jumo 213E)See alsoReferencesNotes=Bibliography * External links * Jumo 213-powered Fw 190D engine startup video * Enginehistory.org's Junkers Jumo 213 page Category:Junkers aircraft engines Category:1940s aircraft piston engines Category:Inverted V12 aircraft engines Category:Inverted aircraft piston engines "