02649cam a2200445Ia 4500100167859MiAaHDL20250726000000.0m d cr bn ---auaua110426e195608 dcua tb f001 0 eng d(MiU)990128618160106381sdr-miu.990128618160106381(MiU)MIU01000000000000012861816-goog(OCoLC)714770174(MiU)Aleph012861816LHLLHLNACARUtOrBLWNACAY 3.N 21/5:15/E56E09ANACA RM E56E09ANovik, David.An analog study of a shock-position diffuser control on a supersonic turbojet engine /David Novik.Washington, D.C. :National Advisory Committee for Aeronautics,1956.27 p. :ill. ;27 cm.texttxtrdacontentunmediatednrdamediavolumencrdacarrierNACA research memorandum ;E56E09ANACA Research Memorandum E56E09A."August 17, 1956."Title from cover.Includes bibliographical references.The effects of diffuser dynamics (for supercritical diffuser operation) and controlled engine dynamics on the diffuser control requirements of a supersonic turbojet engine were studied with the aid of an electronic analog. The investigation indicated that a pressure disturbance in the diffuser had only a small effect on engine speed, whereas a disturbance in engine speed had a large effect on diffuser pressure and could impose severe requirements on diffuser control response.Mode of access: Internet.Charts, diagrams, etc.http://id.loc.gov/authorities/subjects/sh87002373AirplanesTurbojet enginesControl systems.http://id.loc.gov/authorities/subjects/sh85002913AirplanesTurbojet engines.http://id.loc.gov/authorities/subjects/sh85002908Diffusers.http://id.loc.gov/authorities/subjects/sh85037933Lewis Flight Propulsion Laboratory.http://id.loc.gov/authorities/names/no2015026965http://id.loc.gov/rwo/agents/no2015026965http://viaf.org/viaf/314909134United States.National Adviosry Committee for Aeronautics.NACA research memorandum.United States.National Advisory Committee for Aeronautics.http://id.loc.gov/authorities/names/n79060141http://id.loc.gov/rwo/agents/n79060141Technical Report Archive & Image Library (TRAIL)3901508646392710016785920241218054949.020250726000000.020260317165347.02026-03-18T10:01:26Z2024-05-05T17:30:02ZSDR-MIUmiuALMAprepare.pl-004-009BKsdr-miu.990128618160106381MiUSDRGWLA012861816mdp.39015086463927MIU990128618160106381MIUGWLA20260318googlemdp.390150864639271956pdbibUS fed doc