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Matches in DBpedia 2016-04 for { <http://dbpedia.org/resource/Turbojet_development_at_the_RAE> ?p ?o }

• Turbojet_development_at_the_RAE abstract "Between 1936 and 1940 Alan Arnold Griffith designed a series of turbine engines that were built under the direction of Hayne Constant at the Royal Aircraft Establishment (RAE). The designs were advanced for the era, typically featuring a \"two-spool\" layout with high- and low-pressure compressors that individually had more stages than typical engines of the era. Although advanced, the engines were also difficult to build, and only the much simpler \"Freda\" design would ever see production, as the Metrovick F.2 and later the Armstrong Siddeley Sapphire. Much of the pioneering work would be later used in Rolls-Royce designs, starting with the hugely successful Rolls-Royce Avon.".
• Turbojet_development_at_the_RAE wikiPageID "16211966".
• Turbojet_development_at_the_RAE wikiPageLength "14944".
• Turbojet_development_at_the_RAE wikiPageOutDegree "48".
• Turbojet_development_at_the_RAE wikiPageRevisionID "620743145".
• Turbojet_development_at_the_RAE wikiPageWikiLink Advisory_Committee_for_Aeronautics.
• Turbojet_development_at_the_RAE wikiPageWikiLink Aerodynamics.
• Turbojet_development_at_the_RAE wikiPageWikiLink Air_Ministry.
• Turbojet_development_at_the_RAE wikiPageWikiLink Alan_Arnold_Griffith.
• Turbojet_development_at_the_RAE wikiPageWikiLink Angle_of_attack.
• Turbojet_development_at_the_RAE wikiPageWikiLink Armstrong_Siddeley.
• Turbojet_development_at_the_RAE wikiPageWikiLink Armstrong_Siddeley_ASX.
• Turbojet_development_at_the_RAE wikiPageWikiLink Armstrong_Siddeley_Sapphire.
• Turbojet_development_at_the_RAE wikiPageWikiLink Battle_of_Britain.
• Turbojet_development_at_the_RAE wikiPageWikiLink Brown,_Boveri_&_Cie.
• Turbojet_development_at_the_RAE wikiPageWikiLink Category:Jet_engines.
• Turbojet_development_at_the_RAE wikiPageWikiLink Centrifugal_compressor.
• Turbojet_development_at_the_RAE wikiPageWikiLink Compression_ratio.
• Turbojet_development_at_the_RAE wikiPageWikiLink Creep_(deformation).
• Turbojet_development_at_the_RAE wikiPageWikiLink Frank_Whittle.
• Turbojet_development_at_the_RAE wikiPageWikiLink Fuel_efficiency.
• Turbojet_development_at_the_RAE wikiPageWikiLink Gas_generator.
• Turbojet_development_at_the_RAE wikiPageWikiLink General_Electric_Company_plc.
• Turbojet_development_at_the_RAE wikiPageWikiLink Hayne_Constant.
• Turbojet_development_at_the_RAE wikiPageWikiLink Henry_Tizard.
• Turbojet_development_at_the_RAE wikiPageWikiLink Imperial_College_London.
• Turbojet_development_at_the_RAE wikiPageWikiLink Jacob_Ackeret.
• Turbojet_development_at_the_RAE wikiPageWikiLink Mach_number.
• Turbojet_development_at_the_RAE wikiPageWikiLink Metropolitan-Vickers.
• Turbojet_development_at_the_RAE wikiPageWikiLink Metropolitan-Vickers_F.2.
• Turbojet_development_at_the_RAE wikiPageWikiLink NASA.
• Turbojet_development_at_the_RAE wikiPageWikiLink National_Gas_Turbine_Establishment.
• Turbojet_development_at_the_RAE wikiPageWikiLink National_Physical_Laboratory_(United_Kingdom).
• Turbojet_development_at_the_RAE wikiPageWikiLink Overall_pressure_ratio.
• Turbojet_development_at_the_RAE wikiPageWikiLink Power_Jets.
• Turbojet_development_at_the_RAE wikiPageWikiLink Propeller_(aeronautics).
• Turbojet_development_at_the_RAE wikiPageWikiLink Rolls-Royce_Avon.
• Turbojet_development_at_the_RAE wikiPageWikiLink Rolls-Royce_Conway.
• Turbojet_development_at_the_RAE wikiPageWikiLink Rolls-Royce_Limited.
• Turbojet_development_at_the_RAE wikiPageWikiLink Royal_Aircraft_Establishment.
• Turbojet_development_at_the_RAE wikiPageWikiLink Speed_of_sound.
• Turbojet_development_at_the_RAE wikiPageWikiLink Stall_(fluid_mechanics).
• Turbojet_development_at_the_RAE wikiPageWikiLink State_of_the_art.
• Turbojet_development_at_the_RAE wikiPageWikiLink Supercharger.
• Turbojet_development_at_the_RAE wikiPageWikiLink Turbine.
• Turbojet_development_at_the_RAE wikiPageWikiLink Turbofan.
• Turbojet_development_at_the_RAE wikiPageWikiLink Turboprop.
• Turbojet_development_at_the_RAE wikiPageWikiLink Wind_tunnel.
• Turbojet_development_at_the_RAE wikiPageWikiLinkText "Subsequent work at the Royal Aircraft Establishment".
• Turbojet_development_at_the_RAE wikiPageWikiLinkText "Turbojet development at the RAE".
• Turbojet_development_at_the_RAE wikiPageWikiLinkText "a series of designs".
• Turbojet_development_at_the_RAE wikiPageWikiLinkText "developed by the Royal Aeronautical Establishment".
• Turbojet_development_at_the_RAE wikiPageUsesTemplate Template:Convert.
• Turbojet_development_at_the_RAE wikiPageUsesTemplate Template:One_source.
• Turbojet_development_at_the_RAE wikiPageUsesTemplate Template:Reflist.
• Turbojet_development_at_the_RAE subject Category:Jet_engines.
• Turbojet_development_at_the_RAE comment "Between 1936 and 1940 Alan Arnold Griffith designed a series of turbine engines that were built under the direction of Hayne Constant at the Royal Aircraft Establishment (RAE). The designs were advanced for the era, typically featuring a \"two-spool\" layout with high- and low-pressure compressors that individually had more stages than typical engines of the era.".
• Turbojet_development_at_the_RAE label "Turbojet development at the RAE".
• Turbojet_development_at_the_RAE sameAs Q7853898.
• Turbojet_development_at_the_RAE sameAs Q7853898.
• Turbojet_development_at_the_RAE wasDerivedFrom Turbojet_development_at_the_RAE?oldid=620743145.
• Turbojet_development_at_the_RAE isPrimaryTopicOf Turbojet_development_at_the_RAE.