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The Power Jets W.2 was a British turbojet engine designed by Frank Whittle and Power Jets (Research and Development) Ltd. Like the earlier Power Jets W.1, the reverse-flow combustion configuration included a double-sided centrifugal compressor, 10 combustion chambers and an axial-flow turbine with air-cooled disc.

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  • Power Jets W.2 (cs)
  • Power Jets W.2 (fr)
  • Power Jets W.2 (en)
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  • Power Jets W.2 byl britský proudový motor navržený Frankem Whittleyem a . Jako předchozí motor Power Jets W.1 měl podobnou konfiguraci jako protiproudé trubkové spalovací komory, oboustranný radiální kompresor a vzduchem chlazenou část s turbínou. (cs)
  • The Power Jets W.2 was a British turbojet engine designed by Frank Whittle and Power Jets (Research and Development) Ltd. Like the earlier Power Jets W.1, the reverse-flow combustion configuration included a double-sided centrifugal compressor, 10 combustion chambers and an axial-flow turbine with air-cooled disc. (en)
  • Le Power Jets W.2 était un turboréacteur britannique, conçu par Frank Whittle et sa compagnie, la Power Jets (Research and Development) Ltd.. Comme le précédent Power Jets W.1, sa configuration « en trombone » comprenait un compresseur centrifuge unique à double entrée, des chambres de combustion de type reverse flow (à flux inversé) et une turbine axiale refroidie par circulation d'air. (fr)
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  • http://commons.wikimedia.org/wiki/Special:FilePath/Welland.jpg
  • http://commons.wikimedia.org/wiki/Special:FilePath/Whittle_Jet_Engine_W2-700.jpg
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thrust
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turbine
  • Single stage axial flow (en)
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