Results 131 to 140 of about 11,681 (284)

Experimental Investigation of Air-Cooled Turbine Blades in Turbojet Engine. 7: Rotor-Blade Fabrication Procedures [PDF]

open access: yes
An experimental investigation was conducted to determine the cooling effectiveness of a wide variety of air-cooled turbine-blade configurations. The blades, which were tested in the turbine of a - commercial turbojet engine that was modified for this ...
Esgar, Jack B., Long, Roger A.
core   +1 more source

RESEARCH ON APPLICATIONS OF MINI-TURBOJET AND TURBOJET ENGINED MILITARY UAVS

open access: yesSCIENTIFIC RESEARCH AND EDUCATION IN THE AIR FORCE, 2019
Mehmet TURKAY   +4 more
openaire   +1 more source

Experimental verification of principal losses in a regulatory particulate matter emissions sampling system for aircraft turbine engines. [PDF]

open access: yesAerosol Sci Technol, 2021
Kittelson DB   +25 more
europepmc   +1 more source

A generalized computer code for developing dynamic gas turbine engine models (DIGTEM) [PDF]

open access: yes
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

A Preliminary Investigation of the Performance of a Short-length Turbojet Combustor Using Vaporized Hydrocarbon Fuels [PDF]

open access: yes
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

Impact of Biofuel Blends on Black Carbon Emissions from a Gas Turbine Engine. [PDF]

open access: yesEnergy Fuels, 2020
Kumal RR   +19 more
europepmc   +1 more source

Computer simulation of engine systems [PDF]

open access: yes
The use of computerized simulations of the steady state and transient performance of jet engines throughout the flight regime is discussed. In addition, installation effects on thrust and specific fuel consumption is accounted for as well as engine ...
Fishbach, L. H.
core   +1 more source

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