{"title":"粘度对着陆器振动的影响","authors":"A. Panasenko","doi":"10.33257/phchgd.20.4.860","DOIUrl":null,"url":null,"abstract":"The results of preliminary calculations of non-stationary gas flow during the oscillatory movement of the lander at its circular frequency of 2 oscillations per second with the angle of maximum deviation of the symmetry axis from the initial position to one degree in the presence and absence of viscosity effects are presented.","PeriodicalId":309290,"journal":{"name":"Physical-Chemical Kinetics in Gas Dynamics","volume":"30 1","pages":"0"},"PeriodicalIF":0.0000,"publicationDate":"1900-01-01","publicationTypes":"Journal Article","fieldsOfStudy":null,"isOpenAccess":false,"openAccessPdf":"","citationCount":"0","resultStr":"{\"title\":\"Effect of Viscosity on Lander Oscillations\",\"authors\":\"A. Panasenko\",\"doi\":\"10.33257/phchgd.20.4.860\",\"DOIUrl\":null,\"url\":null,\"abstract\":\"The results of preliminary calculations of non-stationary gas flow during the oscillatory movement of the lander at its circular frequency of 2 oscillations per second with the angle of maximum deviation of the symmetry axis from the initial position to one degree in the presence and absence of viscosity effects are presented.\",\"PeriodicalId\":309290,\"journal\":{\"name\":\"Physical-Chemical Kinetics in Gas Dynamics\",\"volume\":\"30 1\",\"pages\":\"0\"},\"PeriodicalIF\":0.0000,\"publicationDate\":\"1900-01-01\",\"publicationTypes\":\"Journal Article\",\"fieldsOfStudy\":null,\"isOpenAccess\":false,\"openAccessPdf\":\"\",\"citationCount\":\"0\",\"resultStr\":null,\"platform\":\"Semanticscholar\",\"paperid\":null,\"PeriodicalName\":\"Physical-Chemical Kinetics in Gas Dynamics\",\"FirstCategoryId\":\"1085\",\"ListUrlMain\":\"https://doi.org/10.33257/phchgd.20.4.860\",\"RegionNum\":0,\"RegionCategory\":null,\"ArticlePicture\":[],\"TitleCN\":null,\"AbstractTextCN\":null,\"PMCID\":null,\"EPubDate\":\"\",\"PubModel\":\"\",\"JCR\":\"\",\"JCRName\":\"\",\"Score\":null,\"Total\":0}","platform":"Semanticscholar","paperid":null,"PeriodicalName":"Physical-Chemical Kinetics in Gas Dynamics","FirstCategoryId":"1085","ListUrlMain":"https://doi.org/10.33257/phchgd.20.4.860","RegionNum":0,"RegionCategory":null,"ArticlePicture":[],"TitleCN":null,"AbstractTextCN":null,"PMCID":null,"EPubDate":"","PubModel":"","JCR":"","JCRName":"","Score":null,"Total":0}
The results of preliminary calculations of non-stationary gas flow during the oscillatory movement of the lander at its circular frequency of 2 oscillations per second with the angle of maximum deviation of the symmetry axis from the initial position to one degree in the presence and absence of viscosity effects are presented.
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