04619nam 22007815 450 991029971310332120200630231836.03-642-54168-210.1007/978-3-642-54168-1(CKB)3710000000089213(EBL)1698232(OCoLC)878564249(SSID)ssj0001186840(PQKBManifestationID)11629600(PQKBTitleCode)TC0001186840(PQKBWorkID)11242752(PQKB)10642363(PQKBManifestationID)16044601(OCoLC)893900416(PQKB)21038260(MiAaPQ)EBC1698232(DE-He213)978-3-642-54168-1(PPN)176751572(EXLCZ)99371000000008921320140222d2014 u| 0engur|n|---|||||txtccrAerodynamic Data of Space Vehicles /by Claus Weiland1st ed. 2014.Berlin, Heidelberg :Springer Berlin Heidelberg :Imprint: Springer,2014.1 online resource (360 p.)Description based upon print version of record.3-642-54167-4 Includes bibliographical references at the end of each chapters and indexes.The Discipline Aerodynamics -- Classi¯cation and Comprehension of Space Vehicles -- Aerothermodynamic Data of Non-winged Re-entry Vehicles (RV-NW)Capsules and Probes -- Erothermodynamic Data of Non-winged Re-entry Vehicles (RV-NW) -- Cones and Bicones.The capacity and quality of the atmospheric flight performance of space flight vehicles is characterized by their aerodynamic data bases. A complete aerodynamic data base would encompass the coefficients of the static longitudinal and lateral motions and the related dynamic coefficients. In this book the aerodynamics of 27 vehicles are considered. Only a few of them did really fly. Therefore the aerodynamic data bases are often not complete, in particular when the projects or programs were more or less abruptly stopped, often due to political decisions. Configurational design studies or the development of demonstrators usually happen with reduced or incomplete aerodynamic data sets. Therefore some data sets base just on the application of one of the following tools: semi-empirical design methods, wind tunnel tests, numerical simulations. In so far a high percentage of the data presented is incomplete and would have to be verified. Flight mechanics needs the aerodynamic coefficients as function of a lot of variables. The allocation of the aerodynamic coefficients for a particular flight operation at a specific trajectory point is conducted by an aerodynamic model. The establishment of such models is described in this book. This book is written for graduate and doctoral students to give them insight into the aerodynamics of the various flight configurations. Further for design and development engineers in industry and at research institutes (including universities) searching for an appropriate vehicle shape, as well as for non-specialists, who may be interested in this subject. The book will be helpful, too, in the case that system studies require in their concept phases the selection of suitable vehicle shapes.Aerospace engineeringAstronauticsFluidsThermodynamicsHeat engineeringHeat transferMass transferAerospace Technology and Astronauticshttps://scigraph.springernature.com/ontologies/product-market-codes/T17050Fluid- and Aerodynamicshttps://scigraph.springernature.com/ontologies/product-market-codes/P21026Engineering Thermodynamics, Heat and Mass Transferhttps://scigraph.springernature.com/ontologies/product-market-codes/T14000Aerospace engineering.Astronautics.Fluids.Thermodynamics.Heat engineering.Heat transfer.Mass transfer.Aerospace Technology and Astronautics.Fluid- and Aerodynamics.Engineering Thermodynamics, Heat and Mass Transfer.532533.62620621.4021Weiland Clausauthttp://id.loc.gov/vocabulary/relators/aut999568BOOK9910299713103321Aerodynamic Data of Space Vehicles2294318UNINA