{"title":"Three-Dimensional Calculation of Double Cone 25°/55° Aerothermodynamics Using a Family of Computer Codes UST3D","authors":"I. A. Koryukov, P. Silvestrov, D. V. Ishin","doi":"10.33257/phchgd.23.2.984","DOIUrl":"https://doi.org/10.33257/phchgd.23.2.984","url":null,"abstract":"A numerical modeling of the three-dimensional flow around a 25°/55° double cone by a high-velocity gas flow on an unstructured grid is carried out. Numerical simulation was carried out in N2 (nitrogen) gas. For numerical simulation, the author's computer codes UST3D-AUSMUP2, UST3D-AUSMPW and USTFEN, developed at IPMech RAS, were used. These computer codes are based on the model of the complete system of Navier-Stokes equations for a perfect gas, which is solved by different methods on an unstructured grid. Validation and verification of the obtained results were carried out. For numerical simulation of the flow, a geometric model of a double cone 25°/55° was constructed.","PeriodicalId":309290,"journal":{"name":"Physical-Chemical Kinetics in Gas Dynamics","volume":"91 1","pages":"0"},"PeriodicalIF":0.0,"publicationDate":"1900-01-01","publicationTypes":"Journal Article","fieldsOfStudy":null,"isOpenAccess":false,"openAccessPdf":"","citationCount":null,"resultStr":null,"platform":"Semanticscholar","paperid":"125002814","PeriodicalName":null,"FirstCategoryId":null,"ListUrlMain":null,"RegionNum":0,"RegionCategory":"","ArticlePicture":[],"TitleCN":null,"AbstractTextCN":null,"PMCID":"","EPubDate":null,"PubModel":null,"JCR":null,"JCRName":null,"Score":null,"Total":0}
{"title":"On Waverider Aerodynamics Experimental Data Analysis Features","authors":"D. Yatsukhno","doi":"10.33257/phchgd.21.2.907","DOIUrl":"https://doi.org/10.33257/phchgd.21.2.907","url":null,"abstract":"The study is devoted to the investigation of the waverider experimental data interpretation. Two features affects the correct comparison opportunity. The first is the virtual and experimental model differences, i.e. the different wetted area. The second is the drag coefficient terms evaluation: pressure drag, skin friction and base drag. The skin friction calculations were performed by the flat plate correlations. The results show that skin friction plays the significant role in the overall drag within the wide Mach number range.","PeriodicalId":309290,"journal":{"name":"Physical-Chemical Kinetics in Gas Dynamics","volume":"10 1","pages":"0"},"PeriodicalIF":0.0,"publicationDate":"1900-01-01","publicationTypes":"Journal Article","fieldsOfStudy":null,"isOpenAccess":false,"openAccessPdf":"","citationCount":null,"resultStr":null,"platform":"Semanticscholar","paperid":"127449170","PeriodicalName":null,"FirstCategoryId":null,"ListUrlMain":null,"RegionNum":0,"RegionCategory":"","ArticlePicture":[],"TitleCN":null,"AbstractTextCN":null,"PMCID":"","EPubDate":null,"PubModel":null,"JCR":null,"JCRName":null,"Score":null,"Total":0}
{"title":"Fine Structure of the Substance Distribution Pattern of a Free - Falling Drop on the Surface and in the Thickness of the Target Fluid in the Impact Mode of Merging","authors":"Y. Chashechkin, A. Ilinykh","doi":"10.33257/phchgd.24.2.1043","DOIUrl":"https://doi.org/10.33257/phchgd.24.2.1043","url":null,"abstract":"","PeriodicalId":309290,"journal":{"name":"Physical-Chemical Kinetics in Gas Dynamics","volume":"4 1","pages":"0"},"PeriodicalIF":0.0,"publicationDate":"1900-01-01","publicationTypes":"Journal Article","fieldsOfStudy":null,"isOpenAccess":false,"openAccessPdf":"","citationCount":null,"resultStr":null,"platform":"Semanticscholar","paperid":"125331224","PeriodicalName":null,"FirstCategoryId":null,"ListUrlMain":null,"RegionNum":0,"RegionCategory":"","ArticlePicture":[],"TitleCN":null,"AbstractTextCN":null,"PMCID":"","EPubDate":null,"PubModel":null,"JCR":null,"JCRName":null,"Score":null,"Total":0}
{"title":"On the Uncertainty of Modeling the Interaction of a Meteoroid with the Atmosphere at Various Entry Velocities","authors":"I. Brykina, L. A. Egorova","doi":"10.33257/phchgd.24.1.1034","DOIUrl":"https://doi.org/10.33257/phchgd.24.1.1034","url":null,"abstract":"","PeriodicalId":309290,"journal":{"name":"Physical-Chemical Kinetics in Gas Dynamics","volume":"22 1","pages":"0"},"PeriodicalIF":0.0,"publicationDate":"1900-01-01","publicationTypes":"Journal Article","fieldsOfStudy":null,"isOpenAccess":false,"openAccessPdf":"","citationCount":null,"resultStr":null,"platform":"Semanticscholar","paperid":"122300701","PeriodicalName":null,"FirstCategoryId":null,"ListUrlMain":null,"RegionNum":0,"RegionCategory":"","ArticlePicture":[],"TitleCN":null,"AbstractTextCN":null,"PMCID":"","EPubDate":null,"PubModel":null,"JCR":null,"JCRName":null,"Score":null,"Total":0}
{"title":"On two-dimensional numerical modeling of the Burrows - Kurkov experimental data on hydrogen combustion in a supersonic air flow usingNS/RANS equations","authors":"Sergey T. Surzhikov","doi":"10.33257/phchgd.22.4.957","DOIUrl":"https://doi.org/10.33257/phchgd.22.4.957","url":null,"abstract":"Using the two-dimensional computer code NERAT-2D, a computational analysis of experimental data on the ignition of a hydrogen jet in a concurrent flow of moist air has been performed. For a numerical study, experimental data were selected [Burrows M.C., Kurkov A.P.] An analytical and experimental study of supersonic combustion of hydrogen in the vitiated air stream. AIAA J. 1973. No.11. Pp. 1217–1218], which have been used for several decades to validate computer codes and physicochemical models of hydrogen combustion in air. Used computer code NERAT-2D implements the numerical integration of two-dimensional Na-vier − Stokes equations on structured multi-block grids. The problem is solved on a sequence of calculation grids without and using Reynolds averaging. The 8-reaction kinetic Evans − Schexnayder model of combustion of molecular hydrogen in hot humid air was used. It is shown that on relatively coarse computational grids, the calculated limit of ignition of a hydrogen jet in an airflow significantly exceeds that measured in the experiment. On detailed computational grids, an unsteady motion of an ignitable hydrogen jet is observed, and the ignition boundary corresponds with good accuracy to the experimental one. As an appendix to the article, a number of animation files are presented that illustrate the unsteady combustion of a hydrogen jet in a co-currents flow of moist air.","PeriodicalId":309290,"journal":{"name":"Physical-Chemical Kinetics in Gas Dynamics","volume":"133 1","pages":"0"},"PeriodicalIF":0.0,"publicationDate":"1900-01-01","publicationTypes":"Journal Article","fieldsOfStudy":null,"isOpenAccess":false,"openAccessPdf":"","citationCount":null,"resultStr":null,"platform":"Semanticscholar","paperid":"117280617","PeriodicalName":null,"FirstCategoryId":null,"ListUrlMain":null,"RegionNum":0,"RegionCategory":"","ArticlePicture":[],"TitleCN":null,"AbstractTextCN":null,"PMCID":"","EPubDate":null,"PubModel":null,"JCR":null,"JCRName":null,"Score":null,"Total":0}
{"title":"Analysis of Two Methods for Estimating the Temperature Dependence of the Gas-Phase Chemical Reactions Rate Constants","authors":"M. F. Danilov","doi":"10.33257/phchgd.24.1.1032","DOIUrl":"https://doi.org/10.33257/phchgd.24.1.1032","url":null,"abstract":"","PeriodicalId":309290,"journal":{"name":"Physical-Chemical Kinetics in Gas Dynamics","volume":"1 1","pages":"0"},"PeriodicalIF":0.0,"publicationDate":"1900-01-01","publicationTypes":"Journal Article","fieldsOfStudy":null,"isOpenAccess":false,"openAccessPdf":"","citationCount":null,"resultStr":null,"platform":"Semanticscholar","paperid":"130414160","PeriodicalName":null,"FirstCategoryId":null,"ListUrlMain":null,"RegionNum":0,"RegionCategory":"","ArticlePicture":[],"TitleCN":null,"AbstractTextCN":null,"PMCID":"","EPubDate":null,"PubModel":null,"JCR":null,"JCRName":null,"Score":null,"Total":0}
{"title":"On the Construction of the Optimal Aerodynamic Design of a High-Speed Aircraft with Specified Payload Geometry","authors":"D. M. Fofonov","doi":"10.33257/phchgd.22.6.965","DOIUrl":"https://doi.org/10.33257/phchgd.22.6.965","url":null,"abstract":"","PeriodicalId":309290,"journal":{"name":"Physical-Chemical Kinetics in Gas Dynamics","volume":"2 1","pages":"0"},"PeriodicalIF":0.0,"publicationDate":"1900-01-01","publicationTypes":"Journal Article","fieldsOfStudy":null,"isOpenAccess":false,"openAccessPdf":"","citationCount":null,"resultStr":null,"platform":"Semanticscholar","paperid":"134060475","PeriodicalName":null,"FirstCategoryId":null,"ListUrlMain":null,"RegionNum":0,"RegionCategory":"","ArticlePicture":[],"TitleCN":null,"AbstractTextCN":null,"PMCID":"","EPubDate":null,"PubModel":null,"JCR":null,"JCRName":null,"Score":null,"Total":0}
{"title":"Approximate Thermal Analysis of Heating and Deformation of a C/C-SiC Plate in a Scramjet Engine","authors":"R. Seleznev, V. Kuzenov","doi":"10.33257/phchgd.24.2.1037","DOIUrl":"https://doi.org/10.33257/phchgd.24.2.1037","url":null,"abstract":"The paper provides a brief overview of heat-resistant materials used by the United States, Germany and Australia the creation of high-speed aircraft. A simplified mathematical model of heating and deformation processes in a C/C-SiC plate based on thermoelasticity equations is formulated. The problem statement is as follows: for a composite plate located on the scramjet engine housing, under given thermal effects and properties of the construction materials, the fields of temperatures, displacements, components of stress and strain tensors are determined. The heating and deformation values in the C/C-SiC plate are estimated.","PeriodicalId":309290,"journal":{"name":"Physical-Chemical Kinetics in Gas Dynamics","volume":"78 6","pages":"0"},"PeriodicalIF":0.0,"publicationDate":"1900-01-01","publicationTypes":"Journal Article","fieldsOfStudy":null,"isOpenAccess":false,"openAccessPdf":"","citationCount":null,"resultStr":null,"platform":"Semanticscholar","paperid":"114039373","PeriodicalName":null,"FirstCategoryId":null,"ListUrlMain":null,"RegionNum":0,"RegionCategory":"","ArticlePicture":[],"TitleCN":null,"AbstractTextCN":null,"PMCID":"","EPubDate":null,"PubModel":null,"JCR":null,"JCRName":null,"Score":null,"Total":0}
{"title":"Results of Supersonic Gas Flow Calculations near AGARD-B Model","authors":"A. Panasenko","doi":"10.33257/phchgd.21.2.887","DOIUrl":"https://doi.org/10.33257/phchgd.21.2.887","url":null,"abstract":"The article presents the results of calculating the aerodynamic characteristics for a supersonic gas flow around the AGARD-B vehicle model at Mach numbers 4 and 5.1 in the range of angles-of-attack 4÷ 9.19.","PeriodicalId":309290,"journal":{"name":"Physical-Chemical Kinetics in Gas Dynamics","volume":"136 1","pages":"0"},"PeriodicalIF":0.0,"publicationDate":"1900-01-01","publicationTypes":"Journal Article","fieldsOfStudy":null,"isOpenAccess":false,"openAccessPdf":"","citationCount":null,"resultStr":null,"platform":"Semanticscholar","paperid":"114284332","PeriodicalName":null,"FirstCategoryId":null,"ListUrlMain":null,"RegionNum":0,"RegionCategory":"","ArticlePicture":[],"TitleCN":null,"AbstractTextCN":null,"PMCID":"","EPubDate":null,"PubModel":null,"JCR":null,"JCRName":null,"Score":null,"Total":0}