Results 81 to 90 of about 49,628 (234)

Analysis of flame stabilization limit in a cylindrical of step micro-combustor with different material through the numerical simulation

MATEC Web of Conferences, 2018
The flame stabilization limit on micro-combustor had studied to support the micro power generator system. Micro-combustion became the crucial components in a micro power generation system as heat resource that will be converted into electricity. However,
Saputro Herman, Purwanto Aris, Fitriana Laila, Wijayanto Danar S, Sutrisno Valiant L P, Ariyanto Eka D, Bima Marshal, Pratama Yuda, Juwantono Heri, Firdani Tutuko, Muslim Riyadi, Munir Fudhail A   +11 more
doaj   +1 more source

Numerical Study on the Solid Fuel Rocket Scramjet Combustor with Cavity

Energies, 2019
Scramjet based on solid propellant is a good supplement for the power device of future hypersonic vehicles. A new scramjet combustor configuration using solid fuel, namely, the solid fuel rocket scramjet (SFRSCRJ) combustor is proposed.
Chaolong Li, Zhixun Xia, Likun Ma, Xiang Zhao, Binbin Chen   +4 more
doaj   +1 more source

Effects of broadened property fuels on radiant heat flux to gas turbine combustor liners [PDF]

The effects of fuel type, inlet air pressure, inlet air temperature, and fuel/air ratio on the combustor radiation were investigated. Combustor liner radiant heat flux measurements were made in the spectral region between 0.14 and 6.5 microns at three ...
Haggard, J. B., Jr.
core   +1 more source

Synchronization framework for modeling transition to thermoacoustic instability in laminar combustors

, 2020
We, herein, present a new model based on the framework of synchronization to describe a thermoacoustic system and capture the multiple bifurcations that such a system undergoes.
Saha, Abhishek, Sujith, R. I., Unni, Vishnu R., Weng, Yue   +3 more
core   +1 more source

The NASA pollution-reduction technology program for small jet aircraft engines [PDF]

Three advanced combustor concepts, designed for the AiResearch TFE 731-2 turbofan engine, were evaluated in screening tests. Goals for carbon monoxide and unburned hydrocarbons were met or closely approached with two of the concepts with relatively ...
Fear, J. S.
core   +1 more source

Combustor liner construction [PDF]

, 1983
A combustor liner is fabricated from a plurality of individual segments each containing counter/parallel Finwall material and are arranged circumferentially and axially to define the combustion zone.
Craig, H. M., Strock, W. J., Wagner, W. B.   +2 more
core   +1 more source

Effect of steam addition on the flow field and NOx emissions for Jet-A in an aircraft combustor [PDF]

, 2016
The steam injection technology for aircraft engines is gaining rising importance because of the strong limitations imposed by the legislation for NOx reduction in airports.
Hu, Chunbo, Nikolaidis, Theoklis, Pilidis, Pericles, Xue, Rui   +3 more
core   +1 more source

Development of low liquid fuel Burnera [PDF]

, 2005
Recently, most of the gas turbine combustion research and development involves in lowering the emissions emitted from the combustor. Emission causes adverse affect to the world and mankind especially. Main concern of the present work is to reduce the NOx
Azeman, Mustafa, Hamidon, Musa, Kamsani, Abdul Majid, Mohamad Shaiful Ashrul, Ishak, Mohd. Jaafar, Mohammad Nazri, Mohd. Zamri, Yusoff, Wan Zaidi, Wan Omar   +6 more
core  

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

Swirl can primary combustor [PDF]

, 1973
A swirl can full annulus combustor, operable over a wide range of exit average temperatures is used in a high performance gas turbine engine for advanced aircraft.
Jones, R. E., Niedzwiecki, R. W.
core   +1 more source