Results 151 to 160 of about 412,817 (220)

Waste to Alternative Fuel: Experimental Investigation of the Effects of Pyrolytic Oil Obtained from Waste Tires, Waste Transformer Oil, and Diesel Fuel Ternary Blends on Engine Performance and Exhaust Emissions in a Diesel Engine. [PDF]

ACS Omega
Yesilyurt MK, Öner İV, Doğan TH, Arpa O, İnce MK.   +4 more
europepmc   +1 more source

Theoretical stress mechanism and structural integrity of viscoelastic propellant grains with variable Poisson's ratio. [PDF]

Sci Rep
Wang X, Wang Y, Qiang H, Bai J, Zhao Z, Luo C.   +5 more
europepmc   +1 more source

Multi-Objective Optimization of Damage Volume and CO₂ Consumption for High-Pressure Liquid CO₂ Jet Impact on Hydroxyl-Terminated Polybutadiene Propellant. [PDF]

Materials (Basel)
Zhang Z, Jiang D, Bai Y, Zhang H, Ding Y.   +4 more
europepmc   +1 more source

Violations of Coordination: Exploring Metastable Diborides via Energetic Transition Metals. [PDF]

J Am Chem Soc
Doane JT, John GM, Kolakji A, Rosenberg AA, Zhang Y, Chen AA, Yeung MT.   +6 more
europepmc   +1 more source

Effects of NO in oxidant and initial temperature on working characteristics of MON-X/MMH liquid space thruster. [PDF]

Sci Prog
Zhou YH, Jiang RP, Li GX, Li HM, Fang T, Tong K.   +5 more
europepmc   +1 more source

Heating rate gradient drives mesostructural dynamics in solid propellant under nonequilibrium conditions. [PDF]

Proc Natl Acad Sci U S A
Jiang Z, Wang T, Sheng W, Li Z, Mao C, Luo H, Xia Y, Shangguan W, Zhang C, Wang J.   +9 more
europepmc   +1 more source

Application of Gaussian SVM Flame Detection Model Based on Color and Gradient Features in Engine Test Plume Images. [PDF]

Sensors (Basel)
Yan S, Gao Y, Zhang Z, Li Y.
europepmc   +1 more source

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Bipropellant combustion in a liquid rocket combustion chamber

Journal of Propulsion and Power, 1992
A comprehensive computer simulation code is developed for the combustion-flow analysis of a bipropellant liquid rocket engine combustor. A bipropellant group combustion model is built in the computer code to facilitate the determination of various combustion modes, including the combustion of oxidizer droplets, fuel droplets and gas mixture.
Tsung Leo Jiang, Huei-Huang Chiu
openaire   +1 more source

Modeling of Rocket Combustion Devices

10th AIAA/ASME Joint Thermophysics and Heat Transfer Conference, 2010
The numerical simulation of the hot-gas side within combustion devices is one important element during the development of today's rocket engines. This paper presents the Astrium hot-gas simulation tool, namely the in-house axisymmetric spray combustion code RocflamII, and shows its validation to experimental subscale data.
Manuel Frey, Thomas Aichner, Josef Görgen, Blazenko Ivancic, Björn Kniesner, Oliver Knab   +5 more
openaire   +1 more source