000 03675nam a22005295i 4500
001 978-3-642-54168-1
003 DE-He213
005 20200421111658.0
007 cr nn 008mamaa
008 140222s2014 gw | s |||| 0|eng d
020 _a9783642541681
_9978-3-642-54168-1
024 7 _a10.1007/978-3-642-54168-1
_2doi
050 4 _aTL787-4050.22
072 7 _aTRP
_2bicssc
072 7 _aTTDS
_2bicssc
072 7 _aTEC002000
_2bisacsh
082 0 4 _a629.1
_223
100 1 _aWeiland, Claus.
_eauthor.
245 1 0 _aAerodynamic Data of Space Vehicles
_h[electronic resource] /
_cby Claus Weiland.
264 1 _aBerlin, Heidelberg :
_bSpringer Berlin Heidelberg :
_bImprint: Springer,
_c2014.
300 _aXVI, 355 p. 403 illus., 269 illus. in color.
_bonline resource.
336 _atext
_btxt
_2rdacontent
337 _acomputer
_bc
_2rdamedia
338 _aonline resource
_bcr
_2rdacarrier
347 _atext file
_bPDF
_2rda
505 0 _aThe 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.
520 _aThe 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.
650 0 _aEngineering.
650 0 _aFluids.
650 0 _aThermodynamics.
650 0 _aHeat engineering.
650 0 _aHeat transfer.
650 0 _aMass transfer.
650 0 _aAerospace engineering.
650 0 _aAstronautics.
650 1 4 _aEngineering.
650 2 4 _aAerospace Technology and Astronautics.
650 2 4 _aFluid- and Aerodynamics.
650 2 4 _aEngineering Thermodynamics, Heat and Mass Transfer.
710 2 _aSpringerLink (Online service)
773 0 _tSpringer eBooks
776 0 8 _iPrinted edition:
_z9783642541674
856 4 0 _uhttp://dx.doi.org/10.1007/978-3-642-54168-1
912 _aZDB-2-ENG
942 _cEBK
999 _c54800
_d54800