More about Flight Propulsion Research Laboratory:
| | Books by Flight Propulsion Research Laboratory: Books in the extended shelves: Flight Propulsion Research Laboratory: Analysis of combustion-chamber performance (National Advisory Committee for Aeronautics, 1948), also by Reece V. Hensley (page images at HathiTrust) Flight Propulsion Research Laboratory: An analysis of control requirements and control parameters for direct-coupled turbojet engines (National Advisory Committee for Aeronautics, 1948), also by David Novik and Edward W. Otto (page images at HathiTrust) Flight Propulsion Research Laboratory: Analysis of turbine performance and effect of tail-pipe design on engine performance (National Advisory Committee for Aeronautics, 1948), also by Richard P. Krebs and Frederick C. Foshag (page images at HathiTrust) Flight Propulsion Research Laboratory: Cooling of gas turbines. [Part] 8, Theoretical temperature distributions through gas turbine with special blades and cooling fins on the rim (National Advisory Committee for Aeronautics, 1948), also by W. Byron Brown and John N. B. Livingood (page images at HathiTrust) Flight Propulsion Research Laboratory: Effect of fuels and fuel-nozzle characteristics on performance of an annular combustor at simulated altitude conditions (National Advisory Committee for Aeronautics, 1948), also by RIchard J. McCafferty (page images at HathiTrust) Flight Propulsion Research Laboratory: Efficiency of radial-flow turbine of turbo engineering corporation TT13-18 turbo super charger (National Advisory Committee for Aeronautics, 1947), also by Earl E. Coulter and William R. Galloway (page images at HathiTrust) Flight Propulsion Research Laboratory: Heat transfer from high-temperature surfaces to fluids. [Part] 1, Preliminary investigation with air in inconel tube with rounded entrance, inside diameter of 0.4 inch and length of 24 inches (National Advisory Committee for Aeronautics, 1948), also by Leroy V. Humble, Milton Grele, Warren H. Lowdermilk, and United States National Advisory Committee for Aeronautics (page images at HathiTrust) Flight Propulsion Research Laboratory: Natural icing of an axial-flow turboject engine in flight for a single icing condition (National Advisory Committee for Aeronautics, 1948), also by Loren W. Acker (page images at HathiTrust) Flight Propulsion Research Laboratory: Operational characteristics (National Advisory Committee for Aeronautics, 1948), also by Richard L. Golladay and Stanley L. Gendler (page images at HathiTrust) Flight Propulsion Research Laboratory: Over-all engine performance (National Advisory Committee for Aeronautics, 1948), also by J. C. Nettles and J. R. Easterly (page images at HathiTrust) Flight Propulsion Research Laboratory: Performance and windmilling drag characteristics (National Advisory Committee for Aeronautics, 1948), also by William A. Fleming (page images at HathiTrust) Flight Propulsion Research Laboratory: Performance of J33 turbojet engine with shaft-power extraction. [Part] 2, Compressor (National Advisory Committee for Aeronautics, 1948), also by Albert O. Ross, J. Cary Nettles, and J. R. Easterly (page images at HathiTrust) Flight Propulsion Research Laboratory: Pressure-sensitive system for gas-temperature control (National Advisory Committee for Aeronautics, 1948), also by Norman Matz and Richard S. Cesaro (page images at HathiTrust) Flight Propulsion Research Laboratory: Ramp floor vent-tube mounting (National Advisory Committee for Aeronautics, 1948), also by Robert S. Ruggeri (page images at HathiTrust) Flight Propulsion Research Laboratory: Some methods of analyzing the effect of basic design variables on axial-flow-compressor performance (National Advisory Committee for Aeronautics, 1947), also by John T. Sinnette (page images at HathiTrust)
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