Results 31 to 40 of about 9,717,661 (350)
Frontiers in Energy Research, 2021 This study was carried out to investigate the loss mechanism of a blade with a harbor seal whisker structure on the trailing edge under different Mach numbers.
Fengbo Wen +4 more
doaj +1 more source
Contribution of Mach number on the evolution of Richtmyer-Meshkov instability induced by shock-accelerated square light bubble [PDF]
Phys. Rev. Fluids 6, 104001 (2021), 2021 The Richtmyer-Meshkov (RM) instability has long been an interesting subject due to its fundamental significance in scientific research, as well as its crucial role in engineering applications. In this study, the contribution of shock Mach number on the evolution of the RM instability induced by a shock-accelerated square light bubble is investigated ...
arxiv +1 more source
Flutter analysis of tapered composite fins: Analysis and experiment [PDF]
FME Transactions, 2022 In the present work, the aeroelastic stability of tapered composite plates is investigated. Existing flutter models, based on the typical section approach, are reviewed for quasi-steady and unsteady low Mach number axial flows and modified for the thin ...
Dinulović Mirko +3 more
doaj +1 more source
A low Mach number solver: Enhancing applicability [PDF]
Journal of Computational Physics, 2013 In astrophysics and meteorology there exist numerous situations where flows exhibit small velocities compared to the sound speed. To overcome the stringent timestep restrictions posed by the predominantly used explicit methods for integration in time the Euler (or Navier-Stokes) equations are usually replaced by modified versions.
Friedrich Kupka +4 more
openaire +2 more sources
Low Mach Number Flows and Combustion [PDF]
SIAM Journal on Mathematical Analysis, 2006 We prove uniform existence results for the full Navier-Stokes equations for time intervals which are independent of the Mach number, the Reynolds number and the P clet number. We consider general equations of state and we give an application for the low Mach number limit combustion problem introduced by Majda.
openaire +5 more sources
Analysis of basic concepts of advanced engines for supersonic civil aircraft on the basis of foreign designers’ experience [PDF]
Вестник Самарского университета: Аэрокосмическая техника, технологии и машиностроение, 2021 The work contains the results of a study of the basic design concepts of advanced engines for supersonic civil aircraft, carried out in order to make a forecast for the development of aviation technology, taking into account the experience of foreign ...
A. D. Alendar +2 more
doaj +1 more source
Electron Surfing and Drift Accelerations in a Weibel-Dominated High-Mach-Number Shock. [PDF]
Physical Review Letters, 2017 How electrons get accelerated to relativistic energies in a high-Mach-number quasiperpendicular shock is presented by means of ab initio particle-in-cell simulations in three dimensions.
Y. Matsumoto +3 more
semanticscholar +1 more source
Modelling interactions between waves and diffused interfaces
International Journal for Numerical Methods in Fluids, Volume 95, Issue 2, Page 215-241, February 2023., 2023 When simulating multiphase compressible flows using the diffuse‐interface methods, important issues arise during the interaction of waves with diffused interfaces. A solution is to use a pressure‐disequilibrium model with finite, instead of infinite, pressure‐relaxation rate.
Kevin Schmidmayer +4 more
wiley +1 more source
On the Low Mach Number Limit for the Compressible Euler System [PDF]
SIAM Journal on Mathematical Analysis, 2018 In this paper, we propose a new approach to singular limits of inviscid fluid flows based on the concept of dissipative measure-valued solutions.
E. Feireisl +2 more
semanticscholar +1 more source
Energy and Exergy Analysis and Optimization of Turbofan Engine-TF30-P414 [PDF]
Iranica Journal of Energy and Environment, 2021 The turbofan engines are one of the constitutes significant components of the aero engines. In this study, the thermodynamic modeling of the TF30-P414 turbofan engine is developed and validated with reference values.
S. D. Farahani +2 more
doaj +1 more source