. . . . . "2485"^^ . . . . . . . . . "Power Jets W.2"@fr . . . . "* Power Jets W.1\n* General Electric I-A\n* Rolls-Royce Welland"@en . "4"^^ . . . . . . . . . . . . . "Le Power Jets W.2 \u00E9tait un turbor\u00E9acteur britannique, con\u00E7u par Frank Whittle et sa compagnie, la Power Jets (Research and Development) Ltd.. Comme le pr\u00E9c\u00E9dent Power Jets W.1, sa configuration \u00AB en trombone \u00BB comprenait un compresseur centrifuge unique \u00E0 double entr\u00E9e, des chambres de combustion de type reverse flow (\u00E0 flux invers\u00E9) et une turbine axiale refroidie par circulation d'air."@fr . . "Kerosene"@en . "Power Jets W.2"@cs . . . "c.1941"@en . . . . . . . "24677697"^^ . . . . . . . "15309"^^ . "1102991074"^^ . "Le Power Jets W.2 \u00E9tait un turbor\u00E9acteur britannique, con\u00E7u par Frank Whittle et sa compagnie, la Power Jets (Research and Development) Ltd.. Comme le pr\u00E9c\u00E9dent Power Jets W.1, sa configuration \u00AB en trombone \u00BB comprenait un compresseur centrifuge unique \u00E0 double entr\u00E9e, des chambres de combustion de type reverse flow (\u00E0 flux invers\u00E9) et une turbine axiale refroidie par circulation d'air."@fr . . . "Power Jets W.2 byl britsk\u00FD proudov\u00FD motor navr\u017Een\u00FD Frankem Whittleyem a . Jako p\u0159edchoz\u00ED motor Power Jets W.1 m\u011Bl podobnou konfiguraci jako protiproud\u00E9 trubkov\u00E9 spalovac\u00ED komory, oboustrann\u00FD radi\u00E1ln\u00ED kompresor a vzduchem chlazenou \u010D\u00E1st s turb\u00EDnou."@cs . . "Single-stage double-sided centrifugal flow"@en . . "Rolls-Royce Derwent"@en . . . . . . "47"^^ . . . . . "Rolls-Royce Welland"@en . . . . "Power Jets W.2"@en . . . . . . . "950.0"^^ . . . "Power Jets W.2 byl britsk\u00FD proudov\u00FD motor navr\u017Een\u00FD Frankem Whittleyem a . Jako p\u0159edchoz\u00ED motor Power Jets W.1 m\u011Bl podobnou konfiguraci jako protiproud\u00E9 trubkov\u00E9 spalovac\u00ED komory, oboustrann\u00FD radi\u00E1ln\u00ED kompresor a vzduchem chlazenou \u010D\u00E1st s turb\u00EDnou."@cs . . . . . . "2.6"^^ . . . . . . . . . "Single stage axial flow"@en . "10"^^ . . . "*List of aircraft engines"@en . . . . . . . . . . . "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 . "Centrifugal flow turbojet"@en . "2610"^^ . . . . . . . "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 . "Jane's"@en .