Results 71 to 80 of about 8,057 (291)

Recent Advances in Non‐Aqueous Liquid Electrolytes for High‐Voltage Sodium‐Ion Batteries

EcoEnergy, EarlyView.
Increasing charging voltage is an effective way to realize sodium‐ion batteries with low cost and high energy density. This review systematically summarizes the development of electrolytes for high‐voltage sodium‐ion batteries in recent years, aiming to promote the breakthrough and application of high energy density sodium‐ion batteries.
Jing Ning, Min Zhou, Yujie Zhang, Tianqi Wang, Manlin Chen, Qiao Cu, Kangli Wang, Wei Wang, Haomiao Li, Kai Jiang   +9 more
wiley   +1 more source

Modeling and Analysis of a LOX/Ethanol Liquid Rocket Engine

Journal of Aerospace Technology and Management, 2018
This work studies the performance and dry mass of the under development LOX/Ethanol L75 liquid rocket engine. To this end, an object-oriented program written in C++ was developed.
Fábio Antônio da Silva Mota, José Nivaldo Hinckel, Evandro Marconi Rocco, Hanfried Schlingloff   +3 more
doaj  

Macroscopic and mesoscopic properties of HTPB propellant under low temperature dynamic biaxial compression loading

Polymer Testing, 2023
In order to study the macroscopic mechanical properties and meso damage mechanism of solid fuel hydroxy-terminated polybutadiene (HTPB) propellant under low temperature and dynamic biaxial compression loading, the INSTRON high strain rate hydraulic ...
Tingjing Geng, Hongfu Qiang, Zhejun Wang, Xueren Wang, Zhaojun Zhu, Dong Qiao   +5 more
doaj  

Intelligent Fault Diagnosis of Liquid Rocket Engine via Interpretable LSTM with Multisensory Data. [PDF]

Sensors (Basel), 2023
Zhang X, Hua X, Zhu J, Ma M.
europepmc   +1 more source

Thermostructural Numerical Analysis of the Thrust Chamber of a Liquid Propellant Rocket Engine. [PDF]

Materials (Basel), 2022
Citarella R, Ferraiuolo M, Perrella M, Giannella V.   +3 more
europepmc   +1 more source

Liquid Rocket Engine.

JAPANESE JOURNAL OF MULTIPHASE FLOW, 1997
PURPOSE:To boost propellant to a high pressure without using a subcombustor by reheating a part of the propellant heated by the heat of a combustor by using a heat exchange means in a nozzle part. CONSTITUTION:The liquid hydrogen as fuel and liquid oxygen as oxidizer are pressurized to each high pressure by boosters 3 and 4.
openaire   +3 more sources

Investigation of the Mechanical Behaviors of Waterborne Polyurethane: The Critical Influence of Hard Segment Content Over Various Strain Rates

Macromolecular Materials and Engineering, EarlyView.
This study explores how hard segment content (HS) modulates waterborne polyureathane's (WPU's) dynamic mechanical properties under low/high strain rates. Increasing HS enhances hydrogen bonding and microphase separation, with abundant hard domains acting as physical crosslinks.
Mingping Zhou, Jiaqiang Xiong, Dingzhe Che, Qiang Wu, Shichao Zhang, Denghui Wang, Fei Gao, Zheng Zhang, Jiping Yang   +8 more
wiley   +1 more source

Prediction of Wall Heat Fluxes in a Rocket Engine with Conjugate Heat Transfer Based on Large-Eddy Simulation. [PDF]

Entropy (Basel), 2022
Potier L, Duchaine F, Cuenot B, Saucereau D, Pichillou J.   +4 more
europepmc   +1 more source

INVESTIGATION OF A GAS-DRIVEN JET PUMP FOR ROCKET ENGINES [PDF]

, 1962
Donald L Crabtree
openalex   +1 more source

Mass Spectrometry Structural Proteomics Enabled by Limited Proteolysis and Cross‐Linking

Mass Spectrometry Reviews, EarlyView.
ABSTRACT The exploration of protein structure and function stands at the forefront of life science and represents an ever‐expanding focus in the development of proteomics. As mass spectrometry (MS) offers readout of protein conformational changes at both the protein and peptide levels, MS‐based structural proteomics is making significant strides in the
Haiyan Lu, Zexin Zhu, Lauren Fields, Hua Zhang, Lingjun Li   +4 more
wiley   +1 more source