Results 111 to 120 of about 22,484 (217)

Thermoelectric hydrogen sensors using Si and SiGe thin films with a catalytic combustor

, 2010
Maiko Nishibori, Woosuck Shin, Noriya Izu, Toshio Itoh, Ichiro Matsubara, Nobuyuki Watanabe, Toshihiro Kasuga   +6 more
openalex   +2 more sources

Hydrogen in transport: a review of opportunities, challenges, and sustainability concerns. [PDF]

RSC Adv
Alreshidi MA, Yadav KK, Shoba G, Gacem A, Padmanabhan S, Ganesan S, Guganathan L, Bhutto JK, Saravanan P, Fallatah AM, Abo El-Khair MA, Almalawi JF, Alam MW, Kavitha C, Tamizhdurai P, Subramani A.   +15 more
europepmc   +1 more source

Numerical Study of the Combustion Characteristics of an 800-1200 kW High-Power Porous Media Combustor at Atmospheric Pressure. [PDF]

ACS Omega
Lin R, Li W, Li H, Liu X, He J, Wang X.
europepmc   +1 more source

Thermal power plant upgrade via a rotating detonation combustor and retrofitted turbine with optimized endwalls

, 2020
Zhe Liu, James Braun, Guillermo Paniagua
openalex   +2 more sources

Investigation of unswept ramp system with lobe shape nozzle for fuel mixing of hydrogen jet at a scramjet engine. [PDF]

Sci Rep
Omar I, El-Sharkawy MR, Ahmed M, Singh PK, Rajab H, Ali R, Ali NB, Rajhi W, Said LB, Abodollahi SA.   +9 more
europepmc   +1 more source

Flammability and Temperature Distributions in a Circulating Fluidized Bed Gas Combustor.

, 1993
Akihiro Kataoka, W. Nowak, Takashi Ihara, Hitoki Matsuda, Masanobu Hasatani, Akira Oda   +5 more
openalex   +2 more sources

Experimental Study of Flame Dynamics in a Triple-Injector Swirling Nonpremixed Combustor Under Different Thermoacoustic Self-Excited Instability Modes. [PDF]

Sensors (Basel)
Zhang X, Wang S, Liu Y.
europepmc   +1 more source

Effect of burner design variables on performance of 16-inch diameter ram-jet combustor using gaseous-hydrogen fuel

, 1957
H George Krull, R. R. Burley
openalex   +1 more source

Combustor and turbine aerothermal interactions in gas turbines with can combustors

, 2016
As the research into the improvement of gas turbine performance progresses, the combustor- turbine interface becomes of increasing importance. In new engine designs components come closer together and the study of the combustor and turbine interactions can prove to be valuable for the improvement of the aerothermal performance of the vane.
openaire   +1 more source

Numerical simulation of premixed n-heptane/air combustion in micro tube with internal channel optimization. [PDF]

Heliyon
Huang Q, Zeng C, Wan W, Chen J, Qiao J.
europepmc   +1 more source