An Experimental Investigation to Use the Biodiesel Resulting from Recycled Sunflower Oil, and Sunflower Oil with Palm Oil as Fuels for Aviation Turbo-Engines. [PDF]
Cican G +4 more
europepmc +1 more source
Toward a second generation fuel efficient supersonic cruise aircraft performance characteristics and benefits [PDF]
The need for greatly improved fuel efficiency and off-design subsonic characteristics is discussed. Engine-airframe matching studies are presented which show the benefits of a configuration designed for much lower supersonic drag levels (blended wing ...
Vachal, J. D.
core +1 more source
Investigation of Combustion of the Gas Turbine Engine from Kerosene and Biokerosene and Their Soot Characteristics in Diffusion Flames. [PDF]
Hong TD +3 more
europepmc +1 more source
Design Optimization of a Gas Turbine Engine for Marine Applications: Off-Design Performance and Control System Considerations. [PDF]
Machmudah A +6 more
europepmc +1 more source
A Preliminary Investigation of the Performance of a Short-length Turbojet Combustor Using Vaporized Hydrocarbon Fuels [PDF]
Two short turbojet combustors designed for use with vaporized hydrocarbon fuels were tested in a one-quarter annular duct. The experimental combustors consisted of many small "swirl-can" combustor elements manifolded together.
Jones, R. E., Pawlik, E. V.
core +1 more source
Experimental verification of principal losses in a regulatory particulate matter emissions sampling system for aircraft turbine engines. [PDF]
Kittelson DB +25 more
europepmc +1 more source
Some aspects of aircraft jet engine fuels [PDF]
Technologies are reviewed for improving the thermal stability of jet fuels, with reference to the overheating of fuel tanks in supersonic aircraft.
Bekiesinski, R.
core +1 more source
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.
core +1 more source
Gear-Shaped High-g Combustion Chamber for Micro Turbojet Engine Applications. [PDF]
Huang H, Chen G, Long H, Lei B, Liang J.
europepmc +1 more source
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.
core +1 more source

