turbofan (Also turbofans) : Related Words Words similar in meaning to turbofan

  • turbojet«
  • fanjet«
  • fan-jet«
  • fanjet engine«
  • turbojet engine«
  • turbofan engine«
  • turbofan«
  • turbo-«
  • pressure ratio«
  • jet engine«
  • engine«
  • unducted fan«
  • fan«
  • jet plane«
  • turboshaft«
  • bypass ratio«
  • jet«
  • net thrust«
  • jet-propelled plane«
  • turboramjet«
  • pratt«
  • turboprop«
  • specific thrust«
  • roll«
  • turbine«
  • afterburner«
  • propjet«
  • hp compressor«
  • turbine inlet temperature«
  • propfan«
  • lp turbine«
  • hp compressor pressure ratio«
  • gas turbine«
  • turbine rotor inlet temperature«
  • compressor«
  • fan pressure ratio«
  • exhaust«
  • thrust«
  • ducted fan«
  • boeing«
  • duct engine«
  • jet noise«
  • core airflow«
  • royce«
  • lp shaft«
  • nozzle«
  • civil engine«
  • core thermal efficiency«
  • whitney«
  • bypass turbofan«
  • modern civil turbofan«
  • royce trent«
  • ip compressor«
  • increase«
  • jet velocity«
  • turbine blade«
  • airflow«
  • turbine system«
  • compression system«
  • core«
  • modern military turbofan«
  • hp turbine rotor inlet temperature«
  • variable geometry«
  • bypass turbofan engine«
  • temperature«
  • general electric«
  • spool configuration«
  • core compression system«
  • air«
  • combustor«
  • specific fuel consumption«
  • mixed exhaust«
  • compressor delivery temperature«
  • snecma«
  • joint venture«
  • flight speed«
  • pressure turbine«
  • nasa innovation«
  • aircraft«
  • stage hp turbine«
  • nozzle pressure ratio«
  • thermal efficiency«
  • stage fan«
  • genx«
  • blade«
  • intermediate pressure«
  • hp turbine«
  • configuration«
  • ip«
  • military engine«
  • engine core«
  • engine cycle«
  • propulsive efficiency«
  • noise«
  • thrust engine«
  • pressure compressor«
  • exhaust velocity«
  • pressure«
  • stage«
  • manufacturer«
  • turbofan engine market«
  • turbine cooling/material technology«
  • thrust growth«
  • sufficient core power«
  • specific thrust/low bypass ratio turbofan«
  • shaft roll«
  • net thrust/intake airflow«
  • modest pressure ratio«
  • medium specific thrust«
  • lp turbine stage«
  • ip compression«
  • hp turbine throat«
  • cold route«
  • blade/vane«
  • gas generator«
  • airstream«
  • body aircraft«
  • bypass«
  • successful commercial jet engine program«
  • main noise source«
  • intake ram drag«
  • core compression«
  • total fuel flow«
  • specific thrust engine«
  • fan thrust«
  • fan match«
  • surge«
  • boeing 767«
  • aft«
  • progress d-436«
  • hot route«
  • core mass flow«
  • average stage loading«
  • speed«
  • shaft turbofan«
  • low specific thrust«
  • ip turbine«
  • final nozzle«
  • fan airflow«
  • modern turbofan«
  • japanese aero engine corporation«
  • power«
  • pure turbojet«
  • whitney jt9d«
  • military turbofan«
  • civil turbofan«
  • whitney f119«
  • overall pressure ratio«
  • propfan engine«
  • engine alliance«
  • fuel efficiency«
  • stage lp turbine«
  • gas turbine research establishment«
  • flight velocity«
  • compressor map«
  • shaft«
  • variable stator«
  • core flow«
  • throat«
  • shear layer«
  • international aero engine«
  • core power«
  • bypass engine«
  • engine pressure ratio«
  • ipc«
  • separate shaft«
  • pure jet«
  • fan diameter«
  • ge90«
  • npo saturn«
  • cfm international«
  • tip speed«
  • fan noise«
  • mtu aero engine«
  • airliner«
  • chevron«
  • ratio«
  • mach«
  • ivchenko«
  • exhaust gas temperature«
  • yakovlev yak-42«
  • ge«
  • klimov«
  • centrifugal«
  • intake«
  • saturn«
  • fan blade«
  • fuel flow«
  • engine model«
  • royce plc«
  • military transport aircraft«
  • mass flow«
  • static pressure«
  • unit«
  • upstream«
  • engine configuration«
  • range«
  • airbus a300«
  • temperature rise«
  • gas turbine engine«
  • e.g.«
  • mechanical energy«
  • airbus a330«
  • airbus a380«
  • rate«
  • parameter«
  • exhaust gas«
  • vane«
  • aerospace industry«
  • efficiency«
  • production«
  • aircraft engine«
  • flow«
  • largest manufacturer«
  • delivery«
  • fuel«
  • low speed«
  • aerodynamics«
  • tit«
  • fleet«
  • williams international«
  • wide scimitar«
  • whitney pw1000g.«
  • whitney jt3c engine«
  • velocity engine exhaust«
  • velocity bypass flow«
  • variable pitch fan blade«
  • ukrainian aircraft engine company«
  • typical 1960s design«
  • turbomachinery configuration«
  • turbojet turbine exhaust«
  • turbojet exhaust jetpipe«
  • turbojet engine noise«
  • turbofan lp compressor«
  • turbofan engine noise propagates«
  • turbofan engine manufacturers«
  • turbo portion«
  • turbine rotor inlet temperature/(hp«
  • turbine rotor entry«
  • turbine blade/vane material«
  • tu-214 series«
  • total fuel flow/net thrust«
  • thrust condition«
  • thrust application«
  • t/o specific thrust«
  • suitable gear ratio«
  • stationary inlet guide vane«
  • spool rb211/trent«
  • specific thrust/high velocity exhaust«
  • specific fuel injector«
  • special mechanical design«
  • soviet ivchenko design bureau«
  • soviet designer arkhip lyulka«
  • sophisticated air cooling scheme«
  • single turbine unit«
  • single hp stage«
  • single fan/gas compressor blade«
  • significant thrust boost«
  • sierra jet«
  • shock wave loss«
  • shear layer turbulence«
  • shallow ip compressor«
  • separate ip turbine«
  • russian turbofan«
  • russian ms-21 airliner«
  • residual shaft power«
  • required fan pressure ratio«
  • recent pratt«
  • ratio compressor«
  • quiet stol aircraft«
  • pw4000 series«
  • propulsive power/rate«
  • propulsive kinetic energy/fuel power«
  • propulsive kinetic energy«
  • pressure ratio ip«
  • pressure fluctuation responsible«
  • power mirage fighter aircraft«
  • power ilyushin il-96«
  • power hal tejas«
  • power boeing«
  • poor propulsive efficiency«
  • poor afterburning sfc/good dry sfc.«
  • peak rits«
  • other noise source«
  • optimum blade speed«
  • nozzle total gross thrust«
  • noise civilian turbofan«
  • newer eagle«
  • new material construction method«
  • multiple axial stage«
  • most modern american civil turbofan«
  • most commercial aviation jet engine«
  • most civil turbofan«
  • modern military turbofan hp compressor«
  • modern military fighter engine«
  • modern general electric f404 fighter engine«
  • mixed nozzle temperature«
  • military turbofans«
  • military kuznetsov nk-25«
  • mcdonnell douglas md-90 family«
  • maximum propulsive efficiency«
  • many turbofan«
  • manufacturer market share«
  • manufacture turbofan«
  • m45sd-02 turbofan«
  • lyulka al-41«
  • lpt blading«
  • lp/ip compression«
  • lp turbine efficiency«
  • lp turbine blade speed«
  • low/medium bypass turbofan«
  • low specific thrust/high bypass ratio turbofan«
  • low bypass ratio turbofan«
  • low bypass ratio military turbofan«
  • lotarev/progress d-18t«
  • lotarev d-36 engine«
  • lockheed c-5 galaxy military transport aircraft«
  • larger rockwell sabreliner«
  • larger ip compressor«
  • larger fan airflow«
  • jet thrust relative«
  • jet outlet velocity«
  • japan aircraft engine company«
  • ipc stage«
  • ipc pressure rise«
  • ip axial stage«
  • interstage/intercompressor«
  • international turbine engine co.«
  • international f-35 lightning ii«
  • intense rotor«
  • integrated aft«
  • improved blade aerodynamics«
  • impossible accurate sensor«
  • ilyushin il-76-md-90«
  • ideal turbine expansion«
  • hpt stator«
  • hp turbine nozzle guide vane«
  • hp mechanical speed«
  • hp compressor delivery temperature«
  • hot mixer entry pressure«
  • hot gas leakage«
  • honeywell htf700 series«
  • honeywell aerospace«
  • gtre)«
  • gtre gtx-35vs kaveri turbofan«
  • general electric turbofan«
  • general electric j85/cj610 turbojet«
  • general electric ge90/genx«
  • ge engine power«
  • gas absolute«
  • fuel:air ratio«
  • fan surge margin«
  • fan rotor stage«
  • fan rotational speed«
  • fan outlet total pressure/intake delivery total pressure«
  • fan hub pressure ratio«
  • fan general electric cf700«
  • fan duct flow/core flow«
  • fan discharge pressure/fan inlet pressure«
  • fan cj805«
  • famous thrust«
  • f124 series«
  • extreme bypass jet engines«
  • extra volume flow«
  • extra core power«
  • extra combustor«
  • equivalent turbofan«
  • engine cycle increase«
  • engine cycle bypass ratio«
  • efficient rotating seal«
  • efficiency edge«
  • early turbojet engine«
  • earliest turbofan«
  • duct loss«
  • duct exhaust system«
  • dry sfc.«
  • downstream turbine blade«
  • downstream lp turbine nozzle guide vane«
  • downstream blades/vanes«
  • critical turbine inlet temperature«
  • core power/power equivalent«
  • core flow/higher bypass ratio cycle«
  • core compression power«
  • constant ׫
  • compressor exit flow function«
  • compressor aerofoil stall«
  • compression inlet airflow«
  • combustor inlet total pressure/intake delivery total pressure«
  • combustor inlet pressure/intake delivery pressure«
  • civilian turbofan engine«
  • civil turbofan derivative«
  • civil general electric cf6 engine«
  • chinese turbofans«
  • cheap jet fuel«
  • cf700 turbofan engine«
  • cf700 aircraft«
  • bypass ratio military turbofan«
  • bypass ratio increase«
  • bypass ratio closer«
  • bypass military turbofan«
  • bypass airstream«
  • british wartime metrovick f.2 axial flow jet«
  • british turbofan«
  • bristol siddeley design«
  • bleed extraction«
  • blade/vane cooling«
  • blade aerodynamics«
  • beechcraft 400xpr«
  • bars/250 psi«
  • apparent air temperature«
  • american turbofan«
  • aircraft fuel reserve«
  • airbus a330 twinjet«
  • aft fan configuration«
  • aeronautics nasa/tm-2011«
  • additional lpt stage«
  • turbo«
  • aeronautics«
  • heat«
  • company«
  • xian ws-15«
  • unmixed turbofan«
  • u civil engine«
  • twin compressor«
  • turbomachinery testing«
  • turbine expansion ratio«
  • thrust size«
  • suiza 12y v-12 piston engine«
  • successful cfm56 series«
  • stator structure«
  • specific thrust turbofan«
  • soviet soloviev design bureau«
  • single fan stage«
  • russian aircraft engine manufacturer«
  • relative airspeed«
  • pressure nature«
  • premier 1a«
  • powerjet«
  • net thrust increase«
  • modern technology aircraft engine«
  • metrovick f.3«
  • lyulka al-31«
  • lp compressor pressure ratio«
  • lower exhaust temperature«
  • lower bypass ratio«
  • low fan pressure ratio«
  • local gas temperature«
  • lf507 turbofan«
  • larger throat«
  • larger temperature drop«
  • klimov rd-33 turbofan engine«
  • joint venture engine«
  • jet noise consideration«
  • jet engine nozzle«
  • ip compressor stage«
  • international aero engines«
  • indirect sensor«
  • ideal maximum«
  • hp turbine blade«
  • hp compression«
  • honeywell international conglomerate«
  • honeywell alf«
  • general electric conglomerate«
  • general electric cfe738«
  • fuel flow/net thrust«
  • fixed total«
  • fixed fuel flow«
  • fan tip«
  • fan mass flow«
  • f414 engine«
  • extra compressor stage«
  • excessive cabin noise«
  • eurojet gmbh«
  • ej200 turbofan engine«
  • duct mode«
  • dry specific thrust«
  • design behaviour«
  • dedicated experimental test rig«
  • common intake«
  • combustor fuel flow«
  • combustor entry temperature«
  • civilian turbofan«
  • civil jetliner«
  • choked nozzle«
  • cessna citationjet cj1«
  • bypass ratio civil turbofan«
  • axial blading«
  • aviadvigatel ps-90 engine«
  • aviadvigatel pd-14 engine«
  • aviadvigatel«
  • assumption invalid«
  • market share«
  • improvement«
  • whitney/allison«
  • variable geometry nozzle«
  • twin engined airliner«
  • tonal noise«
  • spool«
  • special fabrication«
  • sam146«
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