Airplanes -- Turbojet engines -- Combustion chambers -- PerformanceSee also what's at your library, or elsewhere.
Broader terms:Used for:- Performance of turbojet engine combustion chambers
|
Filed under: Airplanes -- Turbojet engines -- Combustion chambers -- Performance- Performance of short length turbojet combustor insensitive to radial distortion of inlet airflow (National Aeronautics and Space Administration ;, 1970), by Francis M. Humenik, United States National Aeronautics and Space Administration, and Lewis Research Center (page images at HathiTrust)
- Photographic studies of preignition environment and flame initiation in turbojet-engine combustors (National Advisory Committee for Aeronautics, 1953), by David M. Straight, J. Dean Gernon, United States National Advisory Committee for Aeronautics, and Lewis Flight Propulsion Laboratory (page images at HathiTrust)
- Simulated altitude performance of two annular combustors with continuous axial openings for admission of primary air (National Advisory Committee for Aeronautics, 1950), by Eugene V. Zettle, Herman Mark, United States National Advisory Committee for Aeronautics, and Lewis Flight Propulsion Laboratory (page images at HathiTrust)
- Performance of experimental channeled-wall annular turbojet combustor at conditions simulating high-altitude supersonic flight. [Part] I, U-shaped channel walls for secondary-air entry / (National Advisory Committee for Aeronautics, 1955), by Eugene V. Zettle, Robert Friedman, Lewis Flight Propulsion Laboratory, United States. National Adviosry Committee for Aeronautics, and United States National Advisory Committee for Aeronautics (page images at HathiTrust)
- Transient and steady-state performance of a single turbojet combustor with four different fuel nozzles (National Advisory Committee for Aeronautics, 1955), by Richard J. McCafferty, Richard H. Donlon, Lewis Flight Propulsion Laboratory, United States. National Adviosry Committee for Aeronautics, and United States National Advisory Committee for Aeronautics (page images at HathiTrust)
- Turbojet combustor performance with injection of hydrogen peroxide for thrust augmentation (National Advisory Committee for Aeronautics, 1956), by Allen J. Metzler, Jack S. Grobman, Lewis Flight Propulsion Laboratory, United States. National Adviosry Committee for Aeronautics, and United States National Advisory Committee for Aeronautics (page images at HathiTrust)
- Simulated afterburner performance with hydrogen peroxide injection for thrust augmentation (National Advisory Committee for Aeronautics, 1956), by Allen J. Metzler, Jack S. Grobman, Lewis Flight Propulsion Laboratory, United States. National Adviosry Committee for Aeronautics, and United States National Advisory Committee for Aeronautics (page images at HathiTrust)
- Effect of combustor-inlet conditions on performance of an annular turbojet combustor (National Advisory Committee for Aeronautics, 1947), by J. Howard Childs, Oakley W. Surine, RIchard J. McCafferty, and United States National Advisory Committee for Aeronautics (page images at HathiTrust)
- Mechanisms of failure of high nickel-alloy turbojet combustion liners (National Advisory Committee for Aeronautics, 1949), by John W. Weeton 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 -- Turbojet engines -- Combustion chambers- NASA TN D-5688 (National Aeronautics and Space Administration ;, 1970), by Richard W. Niedzwiecki, Lewis Research Center, and United States National Aeronautics and Space Administration (page images at HathiTrust)
- Carbon deposition of several special turbojet-engine fuels (National Advisory Committee for Aeronautics, 1951), by Jerrold D. Wear, James W. Useller, United States National Advisory Committee for Aeronautics, and Lewis Flight Propulsion Laboratory (page images at HathiTrust)
- Simulated altitude performance of two annular combustors with continuous axial openings for admission of primary air (National Advisory Committee for Aeronautics, 1950), by Eugene V. Zettle, Herman Mark, United States National Advisory Committee for Aeronautics, and Lewis Flight Propulsion Laboratory (page images at HathiTrust)
- Vapor-fuel-distribution effects on combustion performance of a single tubular combustor (National Advisory Committee for Aeronautics, 1950), by Richard J. McCafferty, United States National Advisory Committee for Aeronautics, and Lewis Flight Propulsion Laboratory (page images at HathiTrust)
- Performance of pure fuels in a single J33 combustor. [Part] III, Five hydrocarbon gaseous fuels and one oxygenated-hydrocarbon gaseous fuel (National Advisory Committee for Aeronautics, 1956), by Arthur L. Smith, Jerrold D. Wear, Lewis Flight Propulsion Laboratory, and United States. National Adviosry Committee for Aeronautics (page images at HathiTrust)
Filed under: Airplanes -- Turbojet engines -- Combustion chambers -- AerodynamicsFiled under: Airplanes -- Turbojet engines -- Combustion chambers -- Testing
Filed under: Airplanes -- Turbojet engines -- Performance- A survey of methods for turbojet thrust measurement applicable to flight installation (National Advisory Committee for Aeronautics, 1955), by William A. Fleming, David S. Gabriel, Lewis Flight Propulsion Laboratory, United States. National Adviosry Committee for Aeronautics, and United States National Advisory Committee for Aeronautics (page images at HathiTrust)
- Equilibrium operating performance of axial-flow turbojet engines by means of idealized analysis (National Advisory Committee for Aeronautics, 1949), by John C. Sanders, Edward C. Chapin, and United States National Advisory Committee for Aeronautics (page images at HathiTrust)
Filed under: Airplanes -- Turbojet engines -- Performance -- TestingFiled under: Airplanes -- Turbojet engines -- Combustion charmbers -- Performance
Filed under: Combustion chambers -- Performance |