Fluid DynamicsPub Date : 2026-09-02DOI: 10.1134/S0015462826605590
S. P. Borisov, A. N. Kudryavtsev
{"title":"Twin Single-Headed Spin Regime of Detonation in a Narrow Rectangular Channel","authors":"S. P. Borisov, A. N. Kudryavtsev","doi":"10.1134/S0015462826605590","DOIUrl":"10.1134/S0015462826605590","url":null,"abstract":"<p>The propagation of a detonation wave in a narrow rectangular channel is numerically simulated. The development of plane detonation wave instability and the formation of an unsteady multifront structure are investigated. An unusual regime of detonation wave propagation with two single-headed spins rotating in opposite directions is detected. It is shown that this mode is unstable: it can exist only for a certain period of time, when the spins rotate synchronously. Its characteristics are investigated, the value of the spin pitch is estimated, and a comparison with the predictions of acoustic theory is made.</p>","PeriodicalId":560,"journal":{"name":"Fluid Dynamics","volume":"61 4","pages":""},"PeriodicalIF":0.7,"publicationDate":"2026-09-02","publicationTypes":"Journal Article","fieldsOfStudy":null,"isOpenAccess":false,"openAccessPdf":"","citationCount":null,"resultStr":null,"platform":"Semanticscholar","paperid":"148926581","PeriodicalName":null,"FirstCategoryId":null,"ListUrlMain":null,"RegionNum":4,"RegionCategory":"工程技术","ArticlePicture":[],"TitleCN":null,"AbstractTextCN":null,"PMCID":"","EPubDate":null,"PubModel":null,"JCR":null,"JCRName":null,"Score":null,"Total":0}
Fluid DynamicsPub Date : 2026-09-02DOI: 10.1134/S0015462826605395
I. G. Brykina, L. A. Egorova
{"title":"Modeling the Interaction of a Meteoroid with the Atmosphere with Variable and Constant Ablation Parameters","authors":"I. G. Brykina, L. A. Egorova","doi":"10.1134/S0015462826605395","DOIUrl":"10.1134/S0015462826605395","url":null,"abstract":"<p>The interaction of a meteoroid and its fragments after disruption with the atmosphere is modeled within the framework of the meteor physics (MF) equations, whose main parameter, along with the drag coefficient, is the ablation parameter equal to the ratio of the heat transfer coefficient to the effective heat of ablation. In the literature, this parameter is usually assumed to be constant and is fitted so that the calculation results correspond to the observation data. In this study under various conditions of body entry into the atmosphere, numerical solutions of the MF equations are obtained both for constant values of the ablation parameter and for a variable ablation parameter determined depending on the body size, the velocity and the flight altitude using correlation formulas previously proposed by the authors. It is studied how using a constant ablation parameter instead of a variable one affects the simulated characteristics: the meteoroid mass loss, the velocity, the energy deposition, and the trajectory, including the prediction of meteorite fall places. The applicability of a constant ablation parameter at various initial velocities, sizes and angles of entry of a cosmic body into the atmosphere is discussed.</p>","PeriodicalId":560,"journal":{"name":"Fluid Dynamics","volume":"61 4","pages":""},"PeriodicalIF":0.7,"publicationDate":"2026-09-02","publicationTypes":"Journal Article","fieldsOfStudy":null,"isOpenAccess":false,"openAccessPdf":"","citationCount":null,"resultStr":null,"platform":"Semanticscholar","paperid":"148926583","PeriodicalName":null,"FirstCategoryId":null,"ListUrlMain":null,"RegionNum":4,"RegionCategory":"工程技术","ArticlePicture":[],"TitleCN":null,"AbstractTextCN":null,"PMCID":"","EPubDate":null,"PubModel":null,"JCR":null,"JCRName":null,"Score":null,"Total":0}
Fluid DynamicsPub Date : 2026-09-02DOI: 10.1134/S0015462826605516
V. G. Lushchik, A. I. Reshmin
{"title":"Delay of Separation of the Turbulent Boundary Layer on a Permeable Plate with Gas Suction in Flow with an Adverse Pressure Gradient","authors":"V. G. Lushchik, A. I. Reshmin","doi":"10.1134/S0015462826605516","DOIUrl":"10.1134/S0015462826605516","url":null,"abstract":"<p>Turbulent flow with an adverse pressure gradient in the boundary layer on a permeable plate with gas suction is studied numerically using a differential three-parameter RANS turbulence model. The study is carried out at a pressure gradient that corresponds to pre-separation boundary layer flow. The calculations made it possible to establish a boundary layer separation criterion on a permeable plate in the range of deceleration and gas suction parameters.</p>","PeriodicalId":560,"journal":{"name":"Fluid Dynamics","volume":"61 4","pages":""},"PeriodicalIF":0.7,"publicationDate":"2026-09-02","publicationTypes":"Journal Article","fieldsOfStudy":null,"isOpenAccess":false,"openAccessPdf":"","citationCount":null,"resultStr":null,"platform":"Semanticscholar","paperid":"148926340","PeriodicalName":null,"FirstCategoryId":null,"ListUrlMain":null,"RegionNum":4,"RegionCategory":"工程技术","ArticlePicture":[],"TitleCN":null,"AbstractTextCN":null,"PMCID":"","EPubDate":null,"PubModel":null,"JCR":null,"JCRName":null,"Score":null,"Total":0}
Fluid DynamicsPub Date : 2026-08-11DOI: 10.1134/S0015462826605413
X. H. Chen, K. Han, H. Li, T. Gao, W. Liu
{"title":"Analysis of the Radial Leakage Flow Field Characteristics of an Asymmetric Micro Scroll Compressor","authors":"X. H. Chen, K. Han, H. Li, T. Gao, W. Liu","doi":"10.1134/S0015462826605413","DOIUrl":"10.1134/S0015462826605413","url":null,"abstract":"<p>In response to the problem of gas leakage in scroll compressors, an asymmetric micro scroll compressor was taken as the research object to construct a radial leakage model of the scroll compressor. The working performance of the scroll compressor under various axial clearances was studied, and the influence of speed and compression ratio on the internal flow field pressure, temperature, speed, and flow rate of the scroll compressor was analyzed. When the axial clearance increases, the pressure, the temperature, the flow rate, and the power of the scroll compressor gradually decrease. In the fluid domain of a scroll compressor, the pressure distribution is uniform, while the temperature and velocity distributions are uneven. As the rotational speed increases, the leakage of the scroll compressor decreases, and the coefficient of variation in the monitoring point temperature decreases from 1.6041 to 1.4301%. The coefficient of variation in the monitoring point velocity decreases from 12.7730 to 8.9128%, and the degree of the uneven temperature and velocity distributions gradually decreases; when the compression ratio increases, the leakage of the scroll compressor increases, and the temperature variation coefficient at the monitoring point increases from 1.5700 to 2.7892%, while the velocity variation coefficient at the monitoring point increases from 11.3075 to 19.9592%. The degree of the uneven temperature and velocity distributions gradually increases. Appropriately increasing the rotational speed and reducing the compression ratio can reduce the leakage of the scroll compressor and minimize the uneven gas temperature and velocity distributions in the compression chamber of the scroll compressor.</p>","PeriodicalId":560,"journal":{"name":"Fluid Dynamics","volume":"61 4","pages":""},"PeriodicalIF":0.7,"publicationDate":"2026-08-11","publicationTypes":"Journal Article","fieldsOfStudy":null,"isOpenAccess":false,"openAccessPdf":"","citationCount":null,"resultStr":null,"platform":"Semanticscholar","paperid":"148699699","PeriodicalName":null,"FirstCategoryId":null,"ListUrlMain":null,"RegionNum":4,"RegionCategory":"工程技术","ArticlePicture":[],"TitleCN":null,"AbstractTextCN":null,"PMCID":"","EPubDate":null,"PubModel":null,"JCR":null,"JCRName":null,"Score":null,"Total":0}
Fluid DynamicsPub Date : 2026-08-11DOI: 10.1134/S0015462826605401
S. N. Vasilieva, I. V. Guk, V. D. Nasonov
{"title":"Experimental Investigation of the Diaphragm Opening in the Gasdynamic CST‑14 System","authors":"S. N. Vasilieva, I. V. Guk, V. D. Nasonov","doi":"10.1134/S0015462826605401","DOIUrl":"10.1134/S0015462826605401","url":null,"abstract":"<p>The results of an of the possibility of shatter-free opening of diaphragms with notches of various depth made of 0.5 mm-thick AMg6M sheet are presented. It is shown that there is a relationship between the notch depth and the diaphragm actuation pressure.</p>","PeriodicalId":560,"journal":{"name":"Fluid Dynamics","volume":"61 4","pages":""},"PeriodicalIF":0.7,"publicationDate":"2026-08-11","publicationTypes":"Journal Article","fieldsOfStudy":null,"isOpenAccess":false,"openAccessPdf":"","citationCount":null,"resultStr":null,"platform":"Semanticscholar","paperid":"148699677","PeriodicalName":null,"FirstCategoryId":null,"ListUrlMain":null,"RegionNum":4,"RegionCategory":"工程技术","ArticlePicture":[],"TitleCN":null,"AbstractTextCN":null,"PMCID":"","EPubDate":null,"PubModel":null,"JCR":null,"JCRName":null,"Score":null,"Total":0}
Fluid DynamicsPub Date : 2026-08-11DOI: 10.1134/S0015462826604237
P. Majumder, H. Dutta, M. R. Choudhury, S. Maity
{"title":"Experimental and Numerical Investigation to Study the Significance of Various Afterbody Shapes for Flow over Bluff Bodies","authors":"P. Majumder, H. Dutta, M. R. Choudhury, S. Maity","doi":"10.1134/S0015462826604237","DOIUrl":"10.1134/S0015462826604237","url":null,"abstract":"<p>The experimental and numerical investigations on the effect of various afterbody shapes on reducing drag and flow over a bluff body are presented. Various after-body parts were generated and experimented to find the drag coefficients with the help of an aerodynamic trainer. Based on the Navier Stokes equation, numerical simulations were performed for those models used in experimental investigation. Four different after-body parts (splitter body, B shape, D shape, and cusped shape) were considered after the square cylinder with an attached thorn at the front of the cylinder and are analysed. The results obtained showed that the cusped shape after the body helps achieve minimum drag as compared to other shapes. Alongside velocity fluctuations, streamlines were also observed both numerically and experimentally to obtain a better scenario about the overall physics of the flow.</p>","PeriodicalId":560,"journal":{"name":"Fluid Dynamics","volume":"61 4","pages":""},"PeriodicalIF":0.7,"publicationDate":"2026-08-11","publicationTypes":"Journal Article","fieldsOfStudy":null,"isOpenAccess":false,"openAccessPdf":"","citationCount":null,"resultStr":null,"platform":"Semanticscholar","paperid":"148699678","PeriodicalName":null,"FirstCategoryId":null,"ListUrlMain":null,"RegionNum":4,"RegionCategory":"工程技术","ArticlePicture":[],"TitleCN":null,"AbstractTextCN":null,"PMCID":"","EPubDate":null,"PubModel":null,"JCR":null,"JCRName":null,"Score":null,"Total":0}
Fluid DynamicsPub Date : 2026-08-11DOI: 10.1134/S001546282660536X
V. Yu. Levashov
{"title":"Influence of the Nucleation Process on the Flow Structure during Unsteady Evaporation","authors":"V. Yu. Levashov","doi":"10.1134/S001546282660536X","DOIUrl":"10.1134/S001546282660536X","url":null,"abstract":"<p>The Boltzmann kinetic equation, the equations of continuum mechanics, and the system of moment equations for homogeneous nucleation are applied to investigate the vapor flow that occurs near a phase interface during its evaporation from a flat surface due to an instantaneous increase of the surface temperature. It is shown that the flow formed as a result of evaporation has a specific structure consisting of several zones. The influence of the bulk vapor condensation on this structure is examined.</p>","PeriodicalId":560,"journal":{"name":"Fluid Dynamics","volume":"61 4","pages":""},"PeriodicalIF":0.7,"publicationDate":"2026-08-11","publicationTypes":"Journal Article","fieldsOfStudy":null,"isOpenAccess":false,"openAccessPdf":"","citationCount":null,"resultStr":null,"platform":"Semanticscholar","paperid":"148699679","PeriodicalName":null,"FirstCategoryId":null,"ListUrlMain":null,"RegionNum":4,"RegionCategory":"工程技术","ArticlePicture":[],"TitleCN":null,"AbstractTextCN":null,"PMCID":"","EPubDate":null,"PubModel":null,"JCR":null,"JCRName":null,"Score":null,"Total":0}
Fluid DynamicsPub Date : 2026-08-11DOI: 10.1134/S0015462826605346
V. V. Kuzenov
{"title":"Obtaining and Regularization of a Hexagonal Irregular Computational Grid","authors":"V. V. Kuzenov","doi":"10.1134/S0015462826605346","DOIUrl":"10.1134/S0015462826605346","url":null,"abstract":"<p>A method for transition from a tetrahedral to a hexagonal irregular computational grid is proposed. A variant of an elliptical grid “regularizer” based on a “mechanical analogy” and solving the linear equations of elasticity theory is developed. The advantages and disadvantages of irregular and regular grids are briefly analyzed. The initial results of reconstruction and “regularization” of the computational grid, as well as the distribution of the “angular” criterion for estimating its quality are given.</p>","PeriodicalId":560,"journal":{"name":"Fluid Dynamics","volume":"61 4","pages":""},"PeriodicalIF":0.7,"publicationDate":"2026-08-11","publicationTypes":"Journal Article","fieldsOfStudy":null,"isOpenAccess":false,"openAccessPdf":"","citationCount":null,"resultStr":null,"platform":"Semanticscholar","paperid":"148699680","PeriodicalName":null,"FirstCategoryId":null,"ListUrlMain":null,"RegionNum":4,"RegionCategory":"工程技术","ArticlePicture":[],"TitleCN":null,"AbstractTextCN":null,"PMCID":"","EPubDate":null,"PubModel":null,"JCR":null,"JCRName":null,"Score":null,"Total":0}
Fluid DynamicsPub Date : 2026-07-19DOI: 10.1134/S0015462826605267
I. V. Sturova, L. A. Tkacheva
{"title":"Hydrodynamic Loads on an Oscillating Circular Cylinder in a Shear-Layer Fluid under Ice Cover","authors":"I. V. Sturova, L. A. Tkacheva","doi":"10.1134/S0015462826605267","DOIUrl":"10.1134/S0015462826605267","url":null,"abstract":"<p>The linear two-dimensional problem of steady-state oscillations of a circular cylinder in the fluid under an ice cover with a shear near-surface layer is solved. The ice cover is modeled by a thin elastic plate of constant thickness. The lower fluid layer contains a circular cylinder oscillating at a given frequency. The presence of the shear layer leads to the appearance of blocking points in the dispersion curves, at which the group velocity of the developing flexural-gravity waves vanishes. The linear approximation becomes unsuitable in the vicinity of these points. Using multipole expansions, the dependences of the hydrodynamic load (added mass and damping coefficients) on the characteristics of the ice cover and shear flow, the oscillation frequency, and the cylinder immersion depth are investigated. It is found that the diagonal added mass coefficients become negative at small distances of the cylinder from the interface and at low oscillation frequencies.</p>","PeriodicalId":560,"journal":{"name":"Fluid Dynamics","volume":"61 3","pages":""},"PeriodicalIF":0.7,"publicationDate":"2026-07-19","publicationTypes":"Journal Article","fieldsOfStudy":null,"isOpenAccess":false,"openAccessPdf":"","citationCount":null,"resultStr":null,"platform":"Semanticscholar","paperid":"148613316","PeriodicalName":null,"FirstCategoryId":null,"ListUrlMain":null,"RegionNum":4,"RegionCategory":"工程技术","ArticlePicture":[],"TitleCN":null,"AbstractTextCN":null,"PMCID":"","EPubDate":null,"PubModel":null,"JCR":null,"JCRName":null,"Score":null,"Total":0}
Fluid DynamicsPub Date : 2026-07-19DOI: 10.1134/S0015462826605334
A. A. Ochirov, Yu. D. Chashechkin
{"title":"Propagation of Two-Dimensional Periodic Surface Disturbances in a Viscous, Continuously Stratified Fluid","authors":"A. A. Ochirov, Yu. D. Chashechkin","doi":"10.1134/S0015462826605334","DOIUrl":"10.1134/S0015462826605334","url":null,"abstract":"<p>The problem of the propagation of two-dimensional periodic flows, including capillary-gravity waves and accompanying perturbations of the free surface of a viscous continuously stratified fluid, is formulated and analyzed using a reduced system of the fundamental equations of fluid mechanics subject to physically substantiated boundary conditions. Spectral equations of motion and dispersion equations for all components of surface flows of a viscous, exponentially stratified fluid are derived for the first time without recourse to the Boussinesq approximation. Complete solutions of the problem include the construction of regular and singular roots of the fourth-order dispersion equation, determining both the waves and the ligaments. In the weak dissipation approximation, the further analysis of the flow properties can be performed numerically or using analytical methods of the united theory of regular and singular perturbations.</p>","PeriodicalId":560,"journal":{"name":"Fluid Dynamics","volume":"61 3","pages":""},"PeriodicalIF":0.7,"publicationDate":"2026-07-19","publicationTypes":"Journal Article","fieldsOfStudy":null,"isOpenAccess":false,"openAccessPdf":"","citationCount":null,"resultStr":null,"platform":"Semanticscholar","paperid":"148613319","PeriodicalName":null,"FirstCategoryId":null,"ListUrlMain":null,"RegionNum":4,"RegionCategory":"工程技术","ArticlePicture":[],"TitleCN":null,"AbstractTextCN":null,"PMCID":"","EPubDate":null,"PubModel":null,"JCR":null,"JCRName":null,"Score":null,"Total":0}