Results 121 to 130 of about 405 (181)
In-situ electrochemical impedance analysis of a commercial SOFC stack fueled by real wood gas. [PDF]
HeliyonTorrigino F +3 more
europepmc +1 more source
Cavitation erosion on different metallic materials under high hydrostatic pressure evaluated with the spatially confined sonoluminescence. [PDF]
Ultrason SonochemLiu Y +8 more
europepmc +1 more source
Some of the next articles are maybe not open access.
Related searches:
Related searches:
Doklady Physics, 2020
For the first time, a detonation afterburner (DA) for continuous detonation combustion of TS-1 aviation kerosene was developed, manufactured, and tested. Test fires of the DA in combination with a TJ100S-125 small-sized single-circuit turbojet engine were carried out on a ground test bench.
S. M. Frolov +10 more
openaire +1 more source
For the first time, a detonation afterburner (DA) for continuous detonation combustion of TS-1 aviation kerosene was developed, manufactured, and tested. Test fires of the DA in combination with a TJ100S-125 small-sized single-circuit turbojet engine were carried out on a ground test bench.
S. M. Frolov +10 more
openaire +1 more source
Afterburner (network-independent card for protocols)
IEEE Network, 1993Many current implementations of protocols such as the Transmission Control Protocol/Internet Protocol (TCP/IP) are inefficient because data are often accessed more frequently than necessary. Three techniques that reduce the need for memory bandwidth are proposed. The techniques are copy-on-write, page remapping, and single-copy.
G Watson
exaly +3 more sources
In-Browser Interactive SQL Analytics with Afterburner
Proceedings of the 2017 ACM International Conference on Management of Data, 2017This demonstration explores the novel and unconventional idea of implementing an analytical RDBMS in pure JavaScript so that it runs completely inside a browser with no external dependencies. Our prototype, called Afterburner, generates compiled query plans that exploit two JavaScript features: typed arrays and asm.js.
Kareem El Gebaly, Jimmy Lin
openaire +2 more sources
2020
Considerable efforts have been made by aero-engine manufacturers to understand, detect, attenuate, if not eliminate, high-frequency transverse screech combustion instabilities due to their destructive nature. Combustion dynamic stability problems arise in turbofan afterburners when fluctuations in the combustion energy release rates are coupled with ...
C. Rajashekar +10 more
openaire +1 more source
Considerable efforts have been made by aero-engine manufacturers to understand, detect, attenuate, if not eliminate, high-frequency transverse screech combustion instabilities due to their destructive nature. Combustion dynamic stability problems arise in turbofan afterburners when fluctuations in the combustion energy release rates are coupled with ...
C. Rajashekar +10 more
openaire +1 more source
Optimization of an industrial afterburner
Journal of Chemometrics, 2003AbstractAn industrial afterburner was optimized using statistical experimental design. A computer‐generated optimal design was adapted to domain constraints and previous knowledge about the experimental variables. Carbon monoxide was used as a general indicator for the operating conditions, and a reduced response surface model was fitted to the ...
openaire +1 more source
Volume 1D, Symposia: Transport Phenomena in Mixing; Turbulent Flows; Urban Fluid Mechanics; Fluid Dynamic Behavior of Complex Particles; Analysis of Elementary Processes in Dispersed Multiphase Flows; Multiphase Flow With Heat/Mass Transfer in Process Technology; Fluid Mechanics of Aircraft and Rocket Emissions and Their Environmental Impacts; High Performance CFD Computation; Performance of Multiphase Flow Systems; Wind Energy; Uncertainty Quantification in Flow Measurements and Simulations, 2014
This paper focuses on two decisive steps towards Large Eddy Simulation of a solid rocket booster jet. First, three-dimensional Large Eddy Simulations of a non-reactive booster jet including the nozzle were obtained at flight conditions of 20 km of altitude.
Adèle Poubeau +2 more
openaire +2 more sources
This paper focuses on two decisive steps towards Large Eddy Simulation of a solid rocket booster jet. First, three-dimensional Large Eddy Simulations of a non-reactive booster jet including the nozzle were obtained at flight conditions of 20 km of altitude.
Adèle Poubeau +2 more
openaire +2 more sources
Afterburners for Turbojet Engines
Journal of the Aeronautical Sciences, 1948The general problem of pure jet aircraft take-off distance is indicated, and the basic reasons for the excess-thrust deficiency as compared to propeller aircraft are shown. The inherent advantages and disadvantages of several methods of short-duration thrust augmentation, such as fluid injection or rocket boosters, to alleviate the difficulties are ...
openaire +1 more source