02675oam 2200781 450 991070972480332120180828112417.0(CKB)5470000002473001(OCoLC)761197631(OCoLC)995470000002473001(EXLCZ)99547000000247300120111115j198604 ua 0engurun||||a|a||txtrdacontentcrdamediacrrdacarrierStatic investigation of two STOL nozzle concepts with pitch thrust-vectoring capability /Mary L. Mason and James R. Burley IIWashington, D.C. :National Aeronautics and Space Administration, Scientific and Technical Information Branch,April 1986.1 online resource (54 pages) illustrationsNASA/TP ;2559"April 1986."Includes bibliographical references (pages 13-14).Nozzle geometrynasatStatic testsnasatNozzle thrust coefficientsnasatAxisymmetric flownasatAfterburningnasatJet nozzlesTestingAirplanesMotorsThrustPitching (Aerodynamics)Short take-off and landing aircraftAirplanesMotorsThrustfastJet nozzlesTestingfastPitching (Aerodynamics)fastShort take-off and landing aircraftfastOnline resources.Nozzle geometry.Static tests.Nozzle thrust coefficients.Axisymmetric flow.Afterburning.Jet nozzlesTesting.AirplanesMotorsThrust.Pitching (Aerodynamics)Short take-off and landing aircraft.AirplanesMotorsThrust.Jet nozzlesTesting.Pitching (Aerodynamics)Short take-off and landing aircraft.Mason Mary L.1407755Burley James R.United States.National Aeronautics and Space Administration.Scientific and Technical Information Branch,Langley Research Center.OCLCEOCLCEOCLCQOCLCFOCLCQOCLCOOCLCQGPOMERUCGPOBOOK9910709724803321Static investigation of two STOL nozzle concepts with pitch thrust-vectoring capability3506423UNINA