Measurement of exhaust emissions from two J-58 engines at simulated supersonic cruise flight conditions [PDF]
Emissions of total oxides of nitrogen, unburned hydrocarbons, carbon monoxide, and carbon dioxide from two J-58 afterburning turbojet engines at simulated high-altitude flight conditions are reported. Test conditions included flight speeds from Mach 2 to
Holdeman, J. D.
core +1 more source
Bibliography on aerodynamics of airframe/engine integration of high-speed turbine-powered aircraft, volume 1 [PDF]
This bibliography was developed as a first step in the preparation of a monograph on the subject of the aerodynamics of airframe/engine integration of high speed turbine powered aircraft.
Nichols, M. R.
core +1 more source
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.
core +1 more source
Health monitoring of the shaft bearings in a micro turbojet based on vibration analysis [PDF]
, 2023 Radosław Przysowa +4 more
openalex +1 more source
Summary of recent investigations of inlet flow distortion effect on engine stability [PDF]
A review is presented of recent experimental results, analytical procedures and test techniques employed to evaluate the effects of inlet flow distortion on the stability characteristics of representative afterburning turbofan and turbojet compression ...
Braithwaite, W. M., Graber, E. J., Jr.
core +1 more source
FSI Application in the Parametric Analysis of Blade–Disk Connection of Turbojet Engine Compressor [PDF]
, 2023 Olga Grzejszczak, Adam Kozakiewicz
openalex +1 more source
Preliminary engineering report for design of a subscale ejector/diffuser system for high expansion ratio space engine testing [PDF]
The design of a subscale jet engine driven ejector/diffuser system is examined. Analytical results and preliminary design drawings and plans are included. Previously developed performance prediction techniques are verified. A safety analysis is performed
Doktor, M. F. +2 more
core +1 more source
Comparative Study of Turbofan and Turbojet Engines [PDF]
, 1957 Benser, W. A. +2 more
core +1 more source