Results 61 to 70 of about 48,816 (291)

Numerical Investigation of Fuel Cooling in Sudden Expansion Structures of Scramjet Engines

open access: yesAerospace
Local overheating in cavities seriously threatens the safe operation of scramjet engines. To investigate the formation mechanism and control methods of local overheating, this paper conducts numerical simulations on the cooling process of cavity sudden ...
Qingjun Wang   +3 more
doaj   +1 more source

Interconnected Porous Hydrogels with Tunable Anisotropy Through Aqueous Emulsion Bioprinting

open access: yesAdvanced Functional Materials, EarlyView.
A 3D bioprintable microporous bioink is developed using an aqueous two‐phase system (ATPS) composed of extracellular matrix (ECM) mimetic biopolymers. The ATPS bioink enables the fabrication of interconnected porous architectures with up to 70% porosity, supporting long‐term cell viability and 3D cell alignment, enabling a simultaneous generation of ...
Hugo Edgar‐Vilar   +4 more
wiley   +1 more source

Numerical simulation on thermal decomposition of n-dodecane using CFD with reaction model

open access: yesJournal of Fluid Science and Technology
A thermal protection makes one of the biggest technical concerns for a reusable hypersonic flight vehicle. A regenerative cooling using fuel should be promising candidate to clear this problem.
Tatsushi ISONO   +4 more
doaj   +1 more source

Conduction Cooling and Plasmonic Heating Dramatically Increase Droplet Vitrification Volumes for Cell Cryopreservation

open access: yesAdvanced Science, 2021
Droplet vitrification has emerged as a promising ice‐free cryopreservation approach to provide a supply chain for off‐the‐shelf cell products in cell therapy and regenerative medicine applications.
Li Zhan   +8 more
doaj   +1 more source

Design of Regenerative Cooled Cryogenic Rocket Engine

open access: yes, 2020
The cryogenic rocket engine using propellants of liquid oxygen (LOX) and also the liquid hydrogen (LH2) category as produces the highest specific impulse has been designed, constructed which comprises of a pressure feed system, injector head assembly thrust chamber, and conical nozzle.
openaire   +1 more source

The Lawrence Berkeley Laboratory geothermal program in northern Nevada [PDF]

open access: yes, 1974
The Lawrence Berkeley Laboratory's geothermal program began with consideration of regions where fluids in the temperature range of 150 to 230 C may be economically accessible.
Mirk, K. F., Wollenberg, H. A.
core   +2 more sources

Viscoelasticity‐Induced Controllable Periodic Meso‐Textures of Liquid Crystal Polymers in Additive Manufacturing

open access: yesAdvanced Functional Materials, EarlyView.
Viscoelasticity‐driven instabilities are harnessed to create tunable, periodic textures in 3D‐printed liquid crystalline polymers. This study illustrates how processing parameters control these spontaneous meso‐scale patterns. These unique structural architectures unlock new possibilities for functional devices, ranging from photonic components to ...
Miaomiao Zou   +17 more
wiley   +1 more source

A regenerative supercritical-subcritical dual-loop organic Rankine cycle system for energy recovery from the waste heat of internal combustion engines [PDF]

open access: yes, 2017
Organic Rankine cycle (ORC) system is considered as a promising technology for energy recovery from the waste heat rejected by internal combustion (IC) engines.
Wang, Enhua   +3 more
core   +1 more source

Adaptive 4D‐Printed Vascular Stents With Low‐Temperature‐Activated and Intelligent Deployment

open access: yesAdvanced Functional Materials, EarlyView.
Microarchitected coronary artery stents were fabricated using a polycaprolactone (PCL)‐based shape memory polymer (SMP) composite via projection micro‐stereolithography (PµSL) 4D printing. By incorporating diethyl phthalate (DEP) as a plasticizer, the thermal transition temperature (Ttran) was modulated to about 37°C, enabling rapid and autonomous ...
Yannan Li   +12 more
wiley   +1 more source

Development and research testing of a low thrust on gaseous-propellant rocket engine chamber

open access: yesВестник Самарского университета: Аэрокосмическая техника, технологии и машиностроение
The article presents preliminary results of the development and research testing of a rocket engine chamber with a thrust of 100 N operating on fuel components: gaseous oxygen-gaseous hydrogen, designed to be used as the main engine of a small upper ...
A. I. Musteikis   +2 more
doaj   +1 more source

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