000 | 03675nam a22005295i 4500 | ||
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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 |
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024 | 7 |
_a10.1007/978-3-642-54168-1 _2doi |
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050 | 4 | _aTL787-4050.22 | |
072 | 7 |
_aTRP _2bicssc |
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072 | 7 |
_aTTDS _2bicssc |
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072 | 7 |
_aTEC002000 _2bisacsh |
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082 | 0 | 4 |
_a629.1 _223 |
100 | 1 |
_aWeiland, Claus. _eauthor. |
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245 | 1 | 0 |
_aAerodynamic Data of Space Vehicles _h[electronic resource] / _cby Claus Weiland. |
264 | 1 |
_aBerlin, Heidelberg : _bSpringer Berlin Heidelberg : _bImprint: Springer, _c2014. |
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300 |
_aXVI, 355 p. 403 illus., 269 illus. in color. _bonline resource. |
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336 |
_atext _btxt _2rdacontent |
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337 |
_acomputer _bc _2rdamedia |
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338 |
_aonline resource _bcr _2rdacarrier |
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347 |
_atext file _bPDF _2rda |
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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 |