Results 1 to 10 of about 148,215 (410)
Improvement of Z-Weighted Function Based on Fifth-Order Nonlinear Multi-Order Weighted Method for Shock Capturing of Hyperbolic Conservation Laws [PDF]
EntropyBased on a 5-point stencil and three 3-point stencils, a nonlinear multi-order weighted method adaptive to 5-3-3-3 stencils for shock capturing is presented in this paper.
Jinwei Bai+4 more
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Transient spray combustion characteristics in a gas–liquid pintle rocket engine under acoustic excitation [PDF]
Scientific ReportsIn order to investigate the acoustic oscillation characteristics of gas–liquid pintle rocket engines and elucidate the path by which spray combustion process provides energy to the combustor pressure oscillation, a LOX/GCH4 pintle engine with rectangular
Xuan Jin+3 more
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Explanation and discovery in aerodynamics [PDF]
arXiv, 2005The purpose of this paper is to discuss and clarify the explanations commonly cited for the aerodynamic lift generated by a wing, and to then analyse, as a case study of engineering discovery, the aerodynamic revolutions which have taken place within Formula 1 in the past 40 years.
McCabe, Gordon
arxiv +4 more sources
Inverse design of aerodynamic configuration using generative topographic mapping
Xibei Gongye Daxue Xuebao, 2022The inverse design method of aerodynamic configuration is hard to give a reasonable pressure distribution, and strongly rely on experience of designers. The method has been difficult to adapt to the needs of modern aircraft design.
SONG Chao+4 more
doaj +1 more source
Aerospace, 2022
The internal weapon bay is widely used in modern aircraft; however, because the unsteady flows of the cavity would cause dangerous store separation and intense aerodynamic noise, the leading-edge spoiler is an easy and efficient passive flow-control ...
Pengcheng Cui+7 more
doaj +1 more source
The internal weapon bay is widely used in modern aircraft; however, because the unsteady flows of the cavity would cause dangerous store separation and intense aerodynamic noise, the leading-edge spoiler is an easy and efficient passive flow-control ...
Pengcheng Cui+7 more
doaj +1 more source
Proceedings of the Royal Society A: Mathematical, Physical and Engineering Sciences, 2014
We study the trajectory of dense projectiles subjected to gravity and drag at large Reynolds number. We show that two types of trajectories can be observed: if the initial velocity is smaller than the terminal velocity of free fall, we observe the classical Galilean parabola: if it is larger, the projectile decelerates with an asymmetric trajectory ...
Cohen, Caroline+5 more
openaire +6 more sources
We study the trajectory of dense projectiles subjected to gravity and drag at large Reynolds number. We show that two types of trajectories can be observed: if the initial velocity is smaller than the terminal velocity of free fall, we observe the classical Galilean parabola: if it is larger, the projectile decelerates with an asymmetric trajectory ...
Cohen, Caroline+5 more
openaire +6 more sources
Aerodynamics of Flying Saucers [PDF]
Communications in Mathematical Physics, 2020We identify various structures on the configuration space C of a flying saucer, moving in a three-dimensional smooth manifold M. Always C is a five-dimensional contact manifold. If M has a projective structure, then C is its twistor space and is equipped with an almost contact Legendrean structure.
Michael Eastwood, Paweł Nurowski
openaire +3 more sources
Journal of Advanced Ceramics, 2022
This work employed an inductively coupled plasma wind tunnel to study the dynamic oxidation mechanisms of carbon fiber reinforced SiC matrix composite (Cf/SiC) in high-enthalpy and high-speed plasmas.
Lingwei Yang+8 more
doaj +1 more source
This work employed an inductively coupled plasma wind tunnel to study the dynamic oxidation mechanisms of carbon fiber reinforced SiC matrix composite (Cf/SiC) in high-enthalpy and high-speed plasmas.
Lingwei Yang+8 more
doaj +1 more source
Journal of Asian Ceramic Societies, 2021
The emissivity of typical SiC-based thermal protection materials was measured in-situ at a wide temperature range (800 ~ 2300°C) inside a plasma wind tunnel that was capable of simulating hypersonic environments on-ground.
Liping Liu+8 more
doaj +1 more source
The emissivity of typical SiC-based thermal protection materials was measured in-situ at a wide temperature range (800 ~ 2300°C) inside a plasma wind tunnel that was capable of simulating hypersonic environments on-ground.
Liping Liu+8 more
doaj +1 more source
Numerical Study of Nonadiabatic Wall Effects on Aerodynamic Characteristics of CHN-T1 Standard Model
Aerospace, 2023Cryogenic wind tunnels provide the for possibility aerodynamic tests to take place over high Reynolds numbers by operating at a low gas temperature to meet the real flight simulation requirements, especially for state-of-the-art large transport aircrafts.
Xiaobing Wang+7 more
doaj +1 more source