Effects of chemical equilibrium on turbine engine performance for various fuels and combustor temperatures [PDF]
A study was performed to quantify the differences in turbine engine performance with and without the chemical dissociation effects for various fuel types over a range of combustor temperatures.
Snyder, Christopher A., Tran, Donald H.
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Variable stream control engine concept for advanced supersonic aircraft: Features and benefits [PDF]
The Variable Stream Control Engine is studied for advanced supersonic cruise aircraft. Significant environmental and performance improvements relative to first generation supersonic turbojet engines are cited.
Howlett, R. A.
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Self-teaching digital-computer program for fail-operational control of a turbojet engine in a sea-level test stand [PDF]
The design and evaluation are described of a digital turbojet engine control which is capable of sensing catastrophic failures in either the engine rotor speed or the compressor discharge static-pressure signal and is capable of switching control modes ...
Arpasi, D. J., Wallhagen, R. E.
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Assessment of a regulatory measurement system for the determination of the non-volatile particulate matter emissions from commercial aircraft engines. [PDF]
J Aerosol Sci, 2021 Kinsey JS +27 more
europepmc +1 more source
RESEARCH ON APPLICATIONS OF MINI-TURBOJET AND TURBOJET ENGINED MILITARY UAVS
SCIENTIFIC RESEARCH AND EDUCATION IN THE AIR FORCE, 2019 Melih Cemal Kuşhan +4 more
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Conditions of generation and methods of damping the inlet vortex of a turbojet engine [PDF]
An aeromechanical analysis of the generation of an inlet vortex in a turbojet engine is presented.
Gajewski, T.
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Discussion: “The MU-CYL-JET: The Multicylinder Turbojet Engine” (Pinnes, R. W., 1962, ASME J. Eng. Power, 84, pp. 131–137) [PDF]
, 1962 Ernest C. Simpson
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Nuclear JT11D-20 Turbojet Engine Estimated Performance 1800F NaK Radiator
, 1960 J. W. Larson
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Data regarding dynamic performance predictions of an aeroengine. [PDF]
Data Brief, 2020 De Giorgi MG, Quarta M.
europepmc +1 more source
HEAVY-LIFT TIP TURBOJET ROTOR SYSTEM. VOLUME 1 [PDF]
, 1965 HILLER AIRCRAFT CORP PALO ALTO CA
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