02524oam 2200685I 450 991070961120332120180613083158.0(CKB)5470000002472128(OCoLC)761342529(EXLCZ)99547000000247212820111115j198504 ua 0engurun||||a|a||txtrdacontentcrdamediacrrdacarrierEffects of inlet distortion on a static pressure probe mounted on the engine hub in an F-15 airplane /Donald L. Hughes, Lawrence P. Myers, and Karen G. MackallWashington, D.C. :National Aeronautics and Space Administration, Scientific and Technical Information Branch,1985.1 online resource (20 pages) illustrationsNASA/TP ;2411"April 1985."Prepared at the Dryden Flight Research Facility.Includes bibliographical references (page 6).Static pressurenasatAircraft enginesnasatInlet flownasatFlight testsnasatPressure measurementnasatStatic pressure probesTestingAirplanesTurbojet enginesAir intakesEagle (Jet fighter plane)AirplanesTurbojet enginesAir intakesfastEagle (Jet fighter plane)fastStatic pressure.Aircraft engines.Inlet flow.Flight tests.Pressure measurement.Static pressure probesTesting.AirplanesTurbojet enginesAir intakes.Eagle (Jet fighter plane)AirplanesTurbojet enginesAir intakes.Eagle (Jet fighter plane)Hughes Donald L(Donald Lee),1926-1410119Myers Lawrence P.Mackall Karen G.United States.National Aeronautics and Space Administration.Scientific and Technical Information Branch,Ames Research Center.Hugh L. Dryden Flight Research Center.OCLCEOCLCEOCLCQOCLCOOCLCQOCLCFGPOBOOK9910709611203321Effects of inlet distortion on a static pressure probe mounted on the engine hub in an F-15 airplane3498168UNINA