Airplanes -- Ramjet engines -- Air intakes -- Testing
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Performance of a translating-double-cone axisymmetric inlet with cowl bypass at mach number from 2.0 to 3.5 (National Advisory Committee for Aeronautics, 1957), by James F. Connors, GeorgeA. Wise, Lewis Flight Propulsion Laboratory, United States. National Adviosry Committee for Aeronautics, and United States National Advisory Committee for Aeronautics (page images at HathiTrust)
Items below (if any) are from related and broader terms.
Filed under: Airplanes -- Ramjet engines -- Air intakes- 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)
- Flight-measured afterbody pressure coefficients from an airplane having twin side-by-side jet engines for Mach numbers from 0.6 to 1.6 (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1979), by Louis L. Steers, Hugh L. Dryden Flight Research Center, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch (page images at HathiTrust)
- Operating characteristics of the Langley Mach 7 Scramjet Test Facility (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1981), by Robert W. Guy, United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch, and Langley Research Center (page images at HathiTrust)
- Expanded operational capabilities of the Langley Mach 7 scramjet test facility (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1983), by Scott R. Thomas, Robert W. Guy, United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch, and Langley 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)
- Free-jet tests of a 1.1-inch-diameter supersonic ram-jet engine (National Advisory Committee for Aeronautics, 1952), by Joseph H. Judd, Otto F. Trout, Langley Aeronautical 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)
- Parametric experimental investigation of a scramjet nozzle at Mach 6 with freon and argon or air used for exhaust simulation (National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division ;, 1991), by James M. Cubbage, William J. Monta, and Langley Research Center (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)
- 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)