Gaseous exhaust emissions from a J-58 engine at simulated supersonic flight conditions [PDF]
Emissions of total oxides of nitrogen, unburned hydrocarbons, carbon monoxide, and carbon dioxide from a J-58 engine at simulated flight conditions of Mach 2.0, 2.4, and 2.8 at 19.8 km altitude are reported.
Holdeman, J. D.
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Application of binary programming to turbojet engine fault detection
, 1987 C A. BOTSARIS +2 more
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Mach 5 inlet CFD and experimental results [PDF]
An experimental research program was conducted in the NASA Lewis Research Center 10 x 10 ft supersonic wind tunnel. The 2-D inlet model was designed to study the Mach 3.0 to 5.0 speed range for an over-under turbojet plus ramjet propulsion system.
Reddy, D. R. +2 more
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Durability of zirconia thermal-barrier ceramic coatings on air-cooled turbine blades in cyclic jet engine operation [PDF]
Thermal barrier ceramic coatings of stabilized zirconia over a bond coat of Ni Cr Al Y were tested for durability on air cooled turbine rotor blades in a research turbojet engine.
Jacobs, R. E. +3 more
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Taking science to cholera in Bangladesh: the personal odyssey of Dr William B Greenough III and his colleagues. [PDF]
eGastroenterology, 2023 Greenough Iii WB +2 more
europepmc +1 more source
A concept for a fuel efficient flight planning aid for general aviation [PDF]
A core equation for estimation of fuel burn from path profile data was developed. This equation was used as a necessary ingredient in a dynamic program to define a fuel efficient flight path.
Collins, B. P. +2 more
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Performance of an annual combustor designed for a low-cost turbojet engine [PDF]
Performance tests were conducted on a combustor designed for use in a low-cost turbojet engine. Low-cost features included the use of very inexpensive simplex fuel nozzles and combustor liners of perforated sheet material.
Fear, J. S.
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Applications of Continuous Fiber Reinforced Ceramic Composites in Military Turbojet Engines [PDF]
, 1996 Patrick Spriet, G. Habarou
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Parametric Analysis of a Turbojet engine with reduced inlet pressure to the compressor
, 2013 A. J. Ujam
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Turbojet and turbofan engines for a mach 3 supersonic transport [PDF]
, 1964 James Dugan +3 more
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