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Airplanes -- Ramjet engines -- Control systems -- Testing

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• Airplanes -- Ramjet engines -- Control systems
• Airplanes -- Ramjet engines -- Testing
• Airplanes -- Control systems -- Testing

• 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.

• Control of Aircraft and Missile Powerplants: An Introduction to the Analysis and Design of Engine Control Systems (New York and London: J. Wiley and Sons, 1963), by Albert J. Sobey and Alfred M. Suggs (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)

• 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)

• 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)

• 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)

• Guidance and control/ACEE. (National Aeronautics and Space Administration :, 1981), by United States National Aeronautics and Space Administration (page images at HathiTrust)
• Flight-test evaluation of STOL control and flight director concepts in a powered-lift aircraft flying curved decelerating approaches (National Aeronautics and Space Admininstration, Scientific and Technical Information Branch ;, 1981), by W. S. Hindson, Robert C. Innis, Gordon H. Hardy, Ames Research Center, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch (page images at HathiTrust)
• Precision controllability of the YF-17 airplane (National Aeronautics and Space Administration, Scientific and Technical Information Office ;, 1980), by Thomas R. Sisk, Neil W. Matheny, Hugh L. Dryden Flight Research Center, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Office (page images at HathiTrust)
• Low-speed wind-tunnel study of reaction control-jet effectiveness for hover and transition of a STOVL fighter concept (National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division ;, 1989), by Donald R. Riley, Gautam H. Shah, Richard E. Kuhn, and Langley Research Center (page images at HathiTrust)
• Dynamics of aircraft antiskid braking systems (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1982), by John A. Tanner, United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch, and Langley Research Center (page images at HathiTrust)
• A simulation study of the flight dynamics of elastic aircraft (National Aeronautics and Space Administration, Scientific and Technical Information Division, 1987), by Martin R. Waszak, D. K. Schmidt, John B. Davidson, and Langley Research Center (page images at HathiTrust)
• NASA TN D-6629 (National Aeronautics and Space Administration :, 1972), by William B. Kemp, Langley Research Center, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Effects of an inset tab on the hinge-moment and effectiveness characteristics of an unswept trailing-edge control on a 60° delta wing at Mach numbers from 0.75 to 1.96 (National Advisory Committee for Aeronautics, 1955), by Lawrence D. Guy, Hoyt V. Brown, and United States National Advisory Committee for Aeronautics (page images at HathiTrust)
• Flight investigation of a small side-located control stick used with electronic control systems in a fighter airplane (National Advisory Committee for Aeronautics, 1957), by S. A. Sjoberg, William L. Alford, Walter R. Russell, and United States National Advisory Committee for Aeronautics (page images at HathiTrust)

• Flight control system design factors for applying automated testing techniques (National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division ;, 1990), by Joel R. Sitz, Todd H. Vernon, and Dryden Flight Research Facility (page images at HathiTrust)

• NASA TN D-1782 (National Aeronautics and Space Administration ;, 1963), by James J. Adams, Langley Research Center, and United States National Aeronautics and Space Administration (page images at HathiTrust; US access only)