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Diffusers

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• Fluid dynamics
• Mechanical engineering

• Mean-flow measurements of the flow field diffusing bend / (Washington, D.C. : National Aeronautics and Space Administration, Scientific and Technical Information Branch ; [Springfield, Va. : For sale by the National Technical Information Service], 1982), by Oden J. McMillan, United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch, Nielsen Engineering & Research, and Lewis Research Center (page images at HathiTrust)
• Preliminary investigation of supersonic diffusers / (Langley Field, VA : Langley Memorial Aeronautical Laboratory, 1945), by Arthur Kantrowitz, Coleman duP. Donaldson, United States. National Advisory Committee for Aeronautics, and Langley Aeronautical Laboratory (page images at HathiTrust)
• Pressure recovery performance of conical diffusers at high subsonic Mach numbers / (Washington, D.C. : National Aeronautics and Space Administration ; [Springfield, Va. : For sale by the National Technical Information Service], 1973), by Francis X. Dolan, Peter W. Runstadler, Lewis Research Center, and inc Creare (page images at HathiTrust)
• Performance of an asymmetric short annular diffuser with a nondiverging inner wall using suction / (Washington, D.C. : National Aeronautics and Space Administration ; [Springfield, Va. : For sale by the National Technical Information Service], 1974), by Albert J. Juhasz and Lewis Research Center (page images at HathiTrust)
• Finite-difference solution for turbulent swirling compressible flow in axisymmetric ducts with struts / (Washington, D.C. : National Aeronautics and Space Administration ; [Springfield, Va. : For sale by the National Technical Information Service], 1974), by O. L. Anderson, Lewis Research Center, and United Aircraft Corporation (page images at HathiTrust)
• Design and experimental performance of short curved wall diffusers with axial symmetry utilizing slot suction / (Washington, D.C. : National Aeronautics and Space Administration ; [Springfield, Va. : For sale by the National Technical Information Service], 1973), by Tah-teh Yang, Carl D. Nelson, William G. Hudson, Lewis Research Center, and Clemson University (page images at HathiTrust)
• Effect of diffusers, shrouds, and mass injection on the starting and operating characteristics of a Mach 5 free jet tunnel / (Washington : National Aeronautics and Space Administration : [For sale by the Clearinghouse for Federal Scientific and Technical Information, Springfield, Va.], 1971), by John K. Molloy, J. Wayne Keyes, Ernest A. Mackley, United States National Aeronautics and Space Administration, and Langley Research Center (page images at HathiTrust)
• Boundary-layer analysis of subsonic inlet diffuser geometries for engine nacelles / (Washington, D.C. : National Aeronautics and Space Administration ; [Springfield, Va. : For sale by the National Technical Information Service], 1974), by James A. Albers, E. John Felderman, and Lewis Research Center (page images at HathiTrust)
• Performance of a low-pressure-ratio centrifugal compressor with four diffuser designs / (Washington, D.C. : National Aeronautics and Space Administration ; [Springfield, Va. : For sale by the National Technical Information Service], 1973), by Hugh A. Klassen and Lewis Research Center (page images at HathiTrust)
• Experimental and analytical study of a conically diffused flow with a nearly separated boundary layer / (Washington, D.C. : National Aeronautics and Space Administration ; [Springfield, Va. : For sale by the National Technical Information Service], 1973), by Donald R. Boldman, Harvey E. Neumann, and Lewis Research Center (page images at HathiTrust)
• Investigations on diffuser efficiency in supersonic wind tunnels = Untersuchungen ueber den diffusorenwirkungsgrad und ueber die erzielung einwandfreier parallelstrahlen bei ueberschallwindkanaelen /, by Klaus Oswatitsch (page images at HathiTrust)
• Report relating to length of outfall and types of diffusers for the ocean outfall for effluent disposal / (Los Angeles : Hyperion Engineers, [1956]), by Koebig & Koebig, Mann Daniel, Holmes & Narver, and Hyperion Engineers (page images at HathiTrust)
• Light shaping diffusers for improved visual inpsection of aircraft / (Washington, D.C. : Federal Aviation Administration, Office of Aviation Research, [1996]), by Richard N. Shagam, Sandia National Laboratories. Aging Aircraft NDI Validation center, and United States. Office of Aviation Research (page images at HathiTrust)
• Comparison of rocket performance using exhaust diffuser and conventional techniques for altitude simulation / (Washington [D.C.] : National Aeronautics and Space Administration, [1959]), by Joseph N. Sivo, Daniel J. Peters, and United States National Aeronautics and Space Administration (page images at HathiTrust; US access only)
• The mixing characteristics of submerged multiple-port diffusers for heated effluents in open channel flow / (Iowa City : University of Iowa, Iowa Institute of Hydraulic Research, [1973]), by John W. Argue, William W. Sayre, Iowa Institute of Hydraulic Research, Commonwealth Edison Company, and United States. Office of Water Resources Research (page images at HathiTrust; US access only)
• Effect of wall suction on performance of a short annular diffuser at inlet Mach numbers up to 0.5 / (Washington, D.C. : National Aeronautics and Space Administration ; [Springfield, Va. : For sale by the National Technical Information Service], 1975), by Albert J. Juhasz and Lewis Research Center (page images at HathiTrust)
• An experimental investigation of two large annular diffusers with swirling and distorted inflow / ([Washington] : National Aeronautics and Space Administration, Scientific and Technical Information Office ; Springfield, Va. : For sale by the National Technical Information Service, 1980), by United States. National Aeronautics and Space Administration. Scientific and Technical Information Office, William T. Eckert, and Aeromechanics Laboratory (page images at HathiTrust)
• Effect of diffuser bleed on performance of an annular swirl can combustor / (Washington, D.C. : National Aeronautics and Space Administration ; [Springfield, Va. : For sale by the National Technical Information Service], 1974), by Albert J. Juhasz and Lewis Research Center (page images at HathiTrust)
• Distortion in a full-scale bicone inlet with internal focused compression and 45 percent internal contraction / (Washington, D.C. : National Aeronautics and Space Administration ; [Springfield, Va. : For sale by the National Technical Information Service], 1974), by Joseph F. Wasserbauer, Robert J. Shaw, Harvey E. Neumann, and Lewis Research Center (page images at HathiTrust)
• Effect of inducer inlet and diffuser throat areas on performance of a low pressure ratio sweptback centrifugal compressor / (Washington, D.C. : National Aeronautics and Space Administration ; [Springfield, Va. : For sale by the National Technical Information Service], 1975), by Hugh A. Klassen and Lewis Research Center (page images at HathiTrust)
• Comparison of experimental and theoretical boundary-layer separation for inlets at incidence angle at low-speed conditions / (Washington, D.C. : National Aeronautics and Space Administration ; [Springfield, Va. : For sale by the National Technical Information Service], 1975), by E. John Felderman, Lewis Research Center, and James A. Albers (page images at HathiTrust)
• Effect of wall edge suction on the performance of a short annular dump diffuser with exit passage flow resistance / (Washington, D.C. : National Aeronautics and Space Administration ; [Springfield, Va. : For sale by the National Technical Information Service], 1975), by Albert J. Juhasz and Lewis Research Center (page images at HathiTrust)
• Preliminary investigation of diffuser wall bleed to control combustor inlet airflow distribution / (Washington, D.C. : National Aeronautics and Space Administration ; Springfield, VA : For sale by the Clearinghouse for Federal Scientific and Technical Information, 1971), by Albert J. Juhasz, J. D. Holdeman, Lewis Research Center, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Performance of high-area-ratio annular dump diffuser using suction-stabilized-vortex flow control / (Washington : National Aeronautics and Space Administration ; Springfield, Va. : For sale by the National Technical Information Service, 1977), by Albert J. Juhasz, John M. Smith, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Performance of a vortex-controlled diffuser in an annular swirl-can combustor at inlet Mach numbers up to 0.53 / ([Washington, D.C.] : National Aeronautics and Space Administration, Scientific and Technical Information Office, 1979), by John M. Smith (page images at HathiTrust)
• Three-dimensional compressible turbulent computations for a diffusing S-duct / (Washington, D.C. : National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program, 1992), by C. F. Smith, Lewis Research Center, and Inc Sverdrup Technology (page images at HathiTrust)
• A Three-dimensional turbulent compressible subsonic duct flow analysis for use with constructed coordinate systems / (Washington, D.C. : National Aeronautics and Space Administration, Scientific and Technical Information Branch ; [Springfield, Va. : For sale by the National Technical Information Service], 1981), by R. Levy, Lewis Research Center, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch (page images at HathiTrust)
• Static tests of an external flow jet augmented flap test bed with a turbojet engine / (Washington, D.C. : National Aeronautics and Space Administration : [For sale by the Office of Technical Services, Dept. of Commerce], [1959]), by Marvin P. Fink and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Report to Hyperion Engineers on methods of analysis of the performance of ocean outfall diffusers with application to the proposed Hyperion outfall / (Pasadena, Calif. : [Hyperion Engineers?, 1956]), by Norman H. Brooks and Hyperion Engineers (page images at HathiTrust; US access only)
• An analog study of a shock-position diffuser control on a supersonic turbojet engine / (Washington, D.C. : National Advisory Committee for Aeronautics, 1956), by David Novik, Lewis Flight Propulsion Laboratory, United States. National Adviosry Committee for Aeronautics. NACA research memorandum, and United States. National Advisory Committee for Aeronautics (page images at HathiTrust)
• An inlet design concept to reduce flow distortion at angle of attack / (Washington, D.C. : National Advisory Committee for Aeronautics, 1957), by Carl F. Schueller, Leonard E. Stitt, Lewis Flight Propulsion Laboratory, United States. National Adviosry Committee for Aeronautics. NACA research memorandum, and United States. National Advisory Committee for Aeronautics (page images at HathiTrust)
• Preliminary investigation of shield to improve angle-of-attack performance of nacelle-type inlet / (Washington, D.C. : National Advisory Committee for Aeronautics, 1957), by Milton A. Beheim, Thomas G. Piercy, Lewis Flight Propulsion Laboratory, and United States. National Adviosry Committee for Aeronautics. NACA research memorandum (page images at HathiTrust)
• Test operation of a prototype, solid-state, helium purification cell /, by R. A. Clark, C. R. Winkelman, B. J. Melton, Los Alamos Scientific Laboratory, and U.S. Atomic Energy Commission (page images at HathiTrust)
• Force and pressure characteristics for a series of nose inlets at Mach numbers from 1.59 to 1.99. (Washington, D.C. : National Advisory Committee for Aeronautics, [1951]), by L. J. Obery, G. W. Englert, United States. National Advisory Committee for Aeronautics. NACA research memorandum, United States. National Advisory Committee for Aeronautics, and Lewis Flight Propulsion Laboratory (page images at HathiTrust)
• Jet diffuser for simulating ram conditions on a turbojet-engine static test stand / (Washington, D.C. : National Advisory Committee for Aeronautics, [1947]), by Robert H. Essig, David S. Gabriel, H. R. Bohanon, United States. National Advisory Committee for Aeronautics. NACA research memorandum, and Aircraft Engine Research Laboratory (page images at HathiTrust)
• Preliminary attempts at isothermal compression of a supersonic air stream / (Washington, D.C. : National Advisory Committee for Aeronautics, [1956]), by E. Perchonok, F. Wilcox, Lewis Flight Propulsion Laboratory, United States. National Adviosry Committee for Aeronautics. NACA research memorandum, and United States. National Advisory Committee for Aeronautics (page images at HathiTrust)
• Performance characteristics of two 6©� and two 12©� diffusers at high flow rates / (Washington, D.C. : National Advisory Committee for Aeronautics, 1949), by William J. Nelson, Eileen G. Popp, Langley Aeronautical Laboratory, and United States. National Adviosry Committee for Aeronautics. NACA research memorandum (page images at HathiTrust)
• The effect of the inlet mach number and inlet-boundary-layer thickness on the performance of a 23©� conical-diffuser-tail-pipe combination / (Washington, D.C. : National Advisory Committee for Aeronautics, 1950), by Jerome Persh, Langley Aeronautical Laboratory, and United States. National Adviosry Committee for Aeronautics. NACA research memorandum (page images at HathiTrust)
• Spectrum of turbulence in a contracting stream / (Washington, D.C. : National Advisory Committee for Aeronautics, 1952), by Herbert Spencer Ribner, Maurice Tucker, and United States. National Advisory Committee for Aeronautics (page images at HathiTrust)
• Performance characteristics of plane-wall two-dimensional diffusers / (Washington, D.C. : National Advisory Committee for Aeronautics, 1953), by Elliott G. Reid and United States. National Advisory Committee for Aeronautics (page images at HathiTrust)
• Air-flow and performance characteristics of engine-stage supercharger of a double-row radial aircraft engine. 2 - Effect of design variables / (Washington, D.C. : National Advisory Committee for Aeronautics, [1946]), by Edmund J. Baas, Paul D. Dugan, Aircraft Engine Research Laboratory, and United States. National Advisory Committee for Aeronautics (page images at HathiTrust)
• Motion of a sphere in a visco-plastic liquid dispersion system /, by N. V. Tyabin, U.S. Atomic Energy Commission, and National Science Foundation (U.S.) (page images at HathiTrust)
• Flow of a visco-plastic dispersion system in a conical diffuser /, by N. V. Tyabin, M. A. Pudovkin, U.S. Atomic Energy Commission, and National Science Foundation (U.S.) (page images at HathiTrust)
• NOL mach 18 hypervelocity research tunnel / (Ft. Belvoir Defense Technical Information Center, 29 AUG 1974), by Ray H. Cornett, Alton G Keel, and Md.) Naval Ordnance Laboratory (White Oak (page images at HathiTrust)
• Subsonic diffuser designs for interceptor applications., by E. David Spong, R. W. Williams, J. V. Rejeske, P. M. Doane, sponsor Air Force Flight Dynamics Laboratory (U.S.), and sponsor McDonnell Aircraft Company (page images at HathiTrust)
• Performance characteristics of a Junkers Jumo 211F engine supercharger with a DVL fully shrouded impeller and scroll diffuser / (Washington, D.C. : National Advisory Committee for Aeronautics, [1945]), by J. Austin King, Harold Klein, Aircraft Engine Research Laboratory, and United States. National Advisory Committee for Aeronautics (page images at HathiTrust)
• Investigation of subsonic duct distortion /, by C. J. MacMiller, sponsor North American Rockwell Corporation, and sponsor Air Force Flight Dynamics Laboratory (U.S.) (page images at HathiTrust)
• Numerical analysis of turbulent separated subsonic diffuser flows /, by J. C. Chien, United States. Air Force. Systems Command. issuing body, sponsor Arnold Engineering Development Center, and Inc. ARO (page images at HathiTrust)
• Numerical computation of subsonic conical diffuser flows with nonuniform turbulent inlet conditions /, by J. C. Chien, United States. Air Force. Systems Command. issuing body, sponsor Arnold Engineering Development Center, and Inc. ARO (page images at HathiTrust)
• Vorticity-stream function formulation of compressible and incompressible turbulent internal flows /, by John C. Chien, Inc. sponsor ARO, United States. Air Force. Arnold Air Force Base. sponsor, and United States. Air Force. Systems Command. Arnold Engineering Development Center. issuing body (page images at HathiTrust)
• Theoretical considerations concerning the flow pattern in a two-dimensional diffuser /, by Karl Gottfried Guderley and issuing agency United States. Army Air Forces. Air Matériel Command (page images at HathiTrust)

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