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Airplanes -- Ramjet engines -- Diffusers

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• Airplanes -- Ramjet engines
• Diffusers

• Airplanes -- Ramjet engines -- Diffusers -- Aerodynamics
• Airplanes -- Ramjet engines -- Diffusers -- Testing

• Supersonic inlet diffusers and introduction to internal aerodynamics. (Minneapolis-Honeywell Regulator Co., Aeronautical Division, 1956), by Rudolf Hermann (page images at HathiTrust)
• Effects of suction boundary-layer control on the performance of a short annular diffuser with an upstream terminal normal shock (National Aeronautics and Space Administration :, 1962), by Charles J. Shoemaker, John R. Henry, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Experimental investigation of direct control of diffuser pressure on 16-inch ram-jet engine (National Advisory Committee for Aeronautics, 1955), by William R. Dunbar, Herbert G. Hurrell, George Vasu, Lewis Flight Propulsion Laboratory, and United States. National Adviosry Committee for Aeronautics (page images at HathiTrust)
• A proposed ram-jet control system operated by use of diffuser pressure recovery (National Advisory Committee for Aeronautics, 1952), by Maxime A. Faget, Langley Aeronautical Laboratory, and United States. National Adviosry Committee for Aeronautics (page images at HathiTrust)

• Dynamic response of a supersonic diffuser to bypass and spike oscillation (National Aeronautics and Space Administration, 1959), by David N. Bowditch, Fred A. Wilcox, and United States National Aeronautics and Space Administration (page images at HathiTrust)

• Application of oblique-shock sensing system to ram-jet-engine flight Mach number control (National Aeronautics and Space Administration, 1955), by Fred A. Wilcox, Donald P. Hearth, Lewis Flight Propulsion Laboratory, United States. National Adviosry Committee for Aeronautics, and United States National Aeronautics and Space Administration (page images at HathiTrust)

Items below (if any) are from related and broader terms.

• Tory II-A mechanical and aero-thermodynamic design ([Lawrence] Radiation Laboratory, 1962), by J. W. Cox, United States. Energy Research and Development Administration, U.S. Atomic Energy Commision, and Livermore. Lawrence Radiation Laboratory University of California (page images at HathiTrust)
• Flight tests of the ramjet on aircraft designed by N. N. Polikarpov in 1939-1940 (Reproduced for NASA by the NASA Scientific and Technical Information Facility, 1968), by A. Ya Shcherbakov (page images at HathiTrust)
• Conceptual study of a turbojet/ramjet inlet (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1979), by John P. Weidner, Langley Research Center, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch (page images at HathiTrust)
• Ignition of mixtures of SiH₄, CH₄, O₂, and Ar or N₂ behind reflected shock waves (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1985), by Allen G. McLain, R. Clayton Rogers, Casimir J. Jachimowski, and Langley Research Center (page images at HathiTrust)
• Effect of ratio of wall boundary-layer thickness to jet diameter on mixing of a normal hydrogen jet in a supersonic stream (National Aeronautics and Space Administration ;, 1974), by Charles R. McClinton and Langley Research Center (page images at HathiTrust)
• Evaluation of bulk calorimeter and heat balance for determination of supersonic combustor efficiency (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1980), by C. R. McClinton, G. Y. Anderson, Langley Research Center, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch (page images at HathiTrust)
• An analysis of combustion studies in shock expansion tunnels and reflected shock tunnels (National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program, 1992), by Casimir J. Jachimowski and Langley Research Center (page images at HathiTrust)
• High-response on-line gas analysis system for hydrogen-reaction combustion products (National Aeronautics and Space Administration ;, 1974), by Allen J. Metzler, Raymond E. Gaugler, and Lewis Research Center (page images at HathiTrust)
• Experimental and analytical study of an inlet forebody for an airframe-integrated scramjet concept (National Aeronautics and Space Administration ;, 1975), by Earl H. Andrews, S. Z. Pinckney, Anthony M. Agnone, and Langley Research Center (page images at HathiTrust)
• Drag and distribution measurements of single-element fuel injectors for supersonic combustors (National Aeronautics and Space Administration ;, 1974), by Louis A. Povinelli and Lewis Research Center (page images at HathiTrust)
• NSEG : a segmented mission analysis program for low and high speed aircraft (National Aeronautics and Space Administration ;, 1977), by D. S. Hague, H. L. Rozendaal, Aerophysics Research Corporation, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Viscous computations of cold air/air flow around scramjet nozzle afterbody (National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program ;, 1991), by Oktay Baysal, Walter C. Englelund, Old Dominion University. Dept. of Mechanical Engineering and Mechanics, and Langley Research Center (page images at HathiTrust)
• Flow analysis and design optimization methods for nozzle afterbody of a hypersonic vehicle (National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program, 1992), by Oktay Baysal, Langley Research Center, and Old Dominion University. Dept. of Mechanical Engineering and Mechanics (page images at HathiTrust)
• Experimental investigation of a Mach 6 fixed-geometry inlet featuring a swept external-internal compression flow field (National Aeronautics and Space Administration ;, 1975), by Marvin G. Torrence and Langley Research Center (page images at HathiTrust)
• Nonreactive mixing study of a scramjet swept-strut fuel injector (National Aeronautics and Space Administration ;, 1975), by Charles R. McClinton and Langley Research Center (page images at HathiTrust)
• Mixing of hydrogen injected from multiple injectors normal to a supersonic airstream (National Aeronautics and Space Administration :, 1971), by R. Clayton Rogers, United States National Aeronautics and Space Administration, and Langley Research Center (page images at HathiTrust)
• NASA TN D-5993 (National Aeronautics and Space Administration :, 1971), by Mark H. Waters and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Upper-stage space-shuttle propulsion by means of separate scramjet and rocket engines (National Aeronautics and Space Administration ;, 1972), by Leo C. Franciscus, John L. Allen, and Lewis Research Center (page images at HathiTrust)
• Exploratory tests of two strut fuel injectors for supersonic combustion (National Aeronautics and Space Administration ;, 1974), by Griffin Y. Anderson, Paul B. Gooderum, and Langley Research Center (page images at HathiTrust)
• Performance of a hydrogen burner to simulate air entering scramjet combustors (National Aeronautics and Space Administration ;, 1974), by William Roger Russin and Langley Research Center (page images at HathiTrust)
• A parametric study of effect of forebody shape on flow angularity at Mach 8 (National Aeronautics and Space Administration ;, 1974), by Charles B. Johnson, Don C. Marcum, and Langley Research Center (page images at HathiTrust)
• Aerodynamic drag and fuel spreading measurements in a simulated scramjet combustion module (National Aeronautics and Space Administration ;, 1974), by Louis A. Povinelli and Lewis Research Center (page images at HathiTrust)
• Diborane, pentaborane, boron, and boron-octene-1 slurries (National Advisory Committee for Aeronautics, 1951), by Benson E. Gammon and United States National Advisory Committee for Aeronautics (page images at HathiTrust; US access only)
• Flight investigation of a ram jet burning magnesium slurry fuel and having a conical shock inlet designed for a Mach number of 4.1 (National Advisory Committee for Aeronautics, 1957), by Walter A. Bartlett, Charles F. Merlet, Langley Aeronautical Laboratory, United States. National Adviosry Committee for Aeronautics, and United States National Advisory Committee for Aeronautics (page images at HathiTrust)
• Analysis of ram-jet engine performance including effects of component changes (National Advisory Committee for Aeronautics, 1956), by Richard J. Weber, Roger W. Luidens, and United States. National Adviosry Committee for Aeronautics (page images at HathiTrust)
• Confidential (Office of the Publication Board, Dept. of Commerce, 1945), by R. L. Sadler, Allied Forces. Supreme Headquarters. Combined Intelligence Objectives Sub-Committee, and United States. Publication Board (page images at HathiTrust)
• Ramjet engines (Liaison Office, Technical Information Center, 1960), by Mikhail Makarovich Bondari͡uk and Sergeĭ Mikhaĭlovich Ilʹi͡ashenko (page images at HathiTrust)
• Coaxial dump ramjet combustor combustion instabilities. Part I. Parametric test data (Wright-Patterson Air Force Base, Ohio : Aero Propulsion Laboratory, Air Force Wright Aeronautical Laboratories, Air Force Systems Command, United States Air Force, 1981., 1981), by D. L. Davis, Air Force Wright Aeronautical Laboratories, and Air Force Aero Propulsion Laboratory (U.S.) (page images at HathiTrust)
• Military jet fuels, 1944-1987 (Wright-Patterson Air Force Base, Ohio : Aero Propulsion Laboratory, Air Force Wright Aeronautical Laboratories, Air Force Systems Command, United States Air Force, 1987., 1987), by Charles R. Martel, Air Force Wright Aeronautical Laboratories, and Air Force Aero Propulsion Laboratory (U.S.) (page images at HathiTrust)
• The use of the p-V-diagram for ramjet calculations (Wright Field, Dayton, Ohio : Headquarters Air Materiel Command, 1947., 1947), by E. R. G. Eckert and United States. Army Air Forces. Air Matériel Command (page images at HathiTrust)
• Handbook of supersonic aerodynamics. Section 17, Ducts, nozzles and diffusers (Silver Spring, Maryland : The Johns Hopkins University, Applied Physics Laboratory, 1964., 1964), by George Rudinger, Johns Hopkins University. Applied Physics Laboratory, and United States Bureau of Naval Weapons (page images at HathiTrust)

• Design and performance at a local Mach number of 6 of an inlet for an integrated scramjet concept (National Aeronautics and Space Administration ;, 1975), by Carl A. Trexler, Sue W. Souders, and Langley Research Center (page images at HathiTrust)
• A forebody design technique for highly integrated botton-mounted scramjets with application to a hypersonic research airplane (National Aeronautics and Space Administration :, 1976), by C. L. W. Edwards and United States National Aeronautics and Space Administration (page images at HathiTrust)
• An analysis of ducted-airfoil ram jets for supersonic aircraft (National Advisory Committee for Aeronautics, 1948), by Paul R. Hill, A. A. Gammal, Langley Aeronautical Laboratory, and United States. National Adviosry Committee for Aeronautics (page images at HathiTrust)
• Method and graphs for the evaluation of air-induction systems (U.S. Government Printing Office, 1953), by George B. Brajnikoff and United States National Advisory Committee for Aeronautics (page images at HathiTrust; US access only)
• Calculation of high speed inlet flows using the Navier-Stokes equations. Volume 1, Description of results / Doyle D. Knight. (Wright-Patterson Air Force Base, Ohio : Air Force Flight Dynamics Laboratory, Air Force Systems Command, United States Air Force, 1980., 1980), by Doyle D. Knight, Air Force Flight Dynamics Laboratory (U.S.), and Rutgers University. Department of Mechanical & Aerospace Engineering (page images at HathiTrust)
• Computer program for design and/or analysis of two-dimensional and axisymmetric inlets (Wright-Patterson Air Force Base : Air Force Flight Dynamics Laboratory, Air Force Wright Aeronautical Laboratories, Air Force Systems Command, 1979., 1979), by Larry K. Ratliff and Air Force Flight Dynamics Laboratory (U.S.) (page images at HathiTrust)
• Subsonic diffuser designs for interceptor applications. Volume II (Wright-Patterson Air Force Base, Ohio : Air Force Flight Dynamics Laboratory, Air Force Systems Command, 1973., 1973), by E. David Spong, R. W. Williams, J. V. Rejeske, P. M. Doane, Air Force Flight Dynamics Laboratory (U.S.), and McDonnell Aircraft Company (page images at HathiTrust)
• Survey of CFD applications for high speed inlets (Wright Patterson Air Force Base, Ohio : Flight Dynamics Directorate , Wright Laboratory, Air Force Materiel Command, United States Air Force, 1994., 1994), by Keith E. Numbers and Ohio) Wright Laboratory (Wright-Patterson Air Force Base (page images at HathiTrust)
• Calculation of high speed inlet flows using the Navier-Stokes equations. Volume II, User's and programmer's guide (Wright-Patterson Air Force Base, Ohio : Air Force Flight Dynamics Laboratory, Air Force Wright Aeronautical Laboratories, Air Force Systems Command, United States Air Force, 1980., 1980), by Doyle D. Knight, Air Force Flight Dynamics Laboratory (U.S.), Air Force Wright Aeronautical Laboratories, and Rutgers University. Department of Mechanical & Aerospace Engineering (page images at HathiTrust)

• Effect of interjet spacing on mixing of multiple coaxial jets in supersonic flow (National Aeronautics and Space Administration ;, 1974), by A. K. Lorber, Joseph A. Schetz, Langley Research Center, and Virginia Polytechnic Institute and State University (page images at HathiTrust)
• Investigation of hydrogen-air ignition senitized by nitric oxide and by nitrogen dioxide (National Aeronautics and Space Administration ;, 1977), by M. Slack, A. Grillo, Grumman Aerospace Corporation, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Method for obtaining aerodynamic data on hypersonic configurations with scramjet exhaust flow simulation (National Aeronautics and Space Administration ;, 1977), by William R. Hartill and United States National Aeronautics and Space Administration (page images at HathiTrust)
• NASA TN D-5315 (National Aeronautics and Space Administration ;, 1969), by James M. Eggers, Marvin G. Torrence, Langley Research Center, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• NASA TN D-5322 (National Aeronautics and Space Administration ;, 1969), by Louis A. Povinelli, Martin Hersch, Frederick P. Povinelli, Lewis Research Center, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Experimental measurements of expanding storable-propellant products simulated by combustion of gaseous reactants (National Aeronautics and Space Administration ;, 1969), by Robert Friedman, Erwin A. Lezberg, Raymond E. Gaugler, United States National Aeronautics and Space Administration, and Lewis Research Center (page images at HathiTrust)
• NASA TN D-6123 (National Aeronautics and Space Administration ;, 1971), by Griffin Y. Anderson, William Roger Russin, Anthony M. Agnone, Langley Research Center, and United States National Aeronautics and Space Administration (page images at HathiTrust; US access only)
• Correlation of secondary sonic and supersonic gaseous jet penetration into supersonic crossflows (National Aeronautics and Space Administration ;, 1971), by Frederick P. Povinelli, Louis A. Povinelli, and Lewis Research Center (page images at HathiTrust)
• Perforated supersonic inlet (National Advisory Committee for Aeronautics, 1948), by Albert H. Schroeder, James F. Connors, United States National Advisory Committee for Aeronautics, and Lewis Flight Propulsion Laboratory (page images at HathiTrust)
• Combustion-chamber performance with four fuels in bumblebee 18-inch ram jet incorporating various rake- or gutter-type flame holders (National Advisory Committee for Aeronautics, 1948), by Ephraim M. Howard, David T. Dupree, Fred A. Wilcox, United States National Advisory Committee for Aeronautics, and Lewis Flight Propulsion Laboratory (page images at HathiTrust)
• Blow-out velocities of several slurry and liquid fuels in a 1 7/8-inch-diameter combustor (National Advisory Committee for Aeronautics, 1955), by James F. Morris, Albert M. Lord, Robert M. Caves, Lewis Flight Propulsion Laboratory, and United States. National Adviosry Committee for Aeronautics (page images at HathiTrust)
• Effect of plastic viscosity and yield value on spray characteristics of magnesium-slurry fuel (National Advisory Committee for Aeronautics, 1957), by George M. Prok, Lewis Flight Propulsion Laboratory, and United States. National Adviosry Committee for Aeronautics (page images at HathiTrust)
• Comparison of the performance of a helicopter-type ram-jet engine under various centrifugal loadings (National Advisory Committee for Aeronautics, 1953), by Edward J. Radin, Paul J. Carpenter, Langley Aeronautical Laboratory, and United States. National Adviosry Committee for Aeronautics (page images at HathiTrust)
• Numerical modelling of ramjet combustors (Wright-Patterson Air Force Base, Ohio : Aero Propulsion Laboratory, Air Force Wright Aeronautical Laboratories, Air Force Systems Command, United States Air Force, 1983., 1983), by Warren H. Harch and Air Force Wright Aeronautical Laboratories (page images at HathiTrust)
• Computation of ramjet internal flowfields (Wright-Patterson Air Force Base, Ohio : Aeropropolsion and Power Laboratory, Wright Research and Development Center, Air Force Systems Command, United States Air Force, 1989., 1989), by James N. Scott, Thomas P. Gielda, Wilbur L. Hankey, University of Dayton, Wright Research and Development Center, Air Force Flight Dynamics Laboratory (U.S.), and United States. Air Force. Systems Command (page images at HathiTrust)

More items available under broader and related terms at left.