Identification and dual adaptive control of a turbojet engine [PDF]
Walter C. Merrill, GARY LELNINGER
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Fuzzy Logic Control of Compressor Surge in a Turbojet Engine Model [PDF]
Mark Laderman
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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]
Kinsey JS+27 more
europepmc +1 more source
A turbojet simulator for Mach numbers up to 2.0 [PDF]
A turbojet simulator was designed and fabricated for use in wind tunnel models. The simulator contains a six-stage, axial-flow compressor powered by a three-stage, axial-flow turbine. High pressure heated air was used to drive the turbine.
Nosek, S. M.+3 more
core +1 more source
RESEARCH ON APPLICATIONS OF MINI-TURBOJET AND TURBOJET ENGINED MILITARY UAVS
Melih Cemal Kuşhan+4 more
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Investigation of thrust vector angle control law based on micro-turbojet engine [PDF]
Shaoqing Chi+3 more
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A generalized computer code for developing dynamic gas turbine engine models (DIGTEM) [PDF]
This paper describes DIGTEM (digital turbofan engine model), a computer program that simulates two spool, two stream (turbofan) engines. DIGTEM was developed to support the development of a real time multiprocessor based engine simulator being designed ...
Daniele, C. J.
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Transient Behavior in Variable Geometry Industrial Gas Turbines: A Comprehensive Overview of Pertinent Modeling Techniques. [PDF]
Hashmi MB, Lemma TA, Ahsan S, Rahman S.
europepmc +1 more source
Emission calibration of a J-58 afterburning turbojet engine at simulated supersonic stratospheric flight conditions [PDF]
Emissions of total oxides of nitrogen, unburned hydrocarbons, and carbon monoxide 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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Study on Microwave-Assisted Ignition Using a Novel Aero-Engine Combustor. [PDF]
Zhang Y, Zhao B, He L, Zeng H, Chang Y.
europepmc +1 more source