000 | 03384nam a22005655i 4500 | ||
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001 | 978-3-319-46055-0 | ||
003 | DE-He213 | ||
005 | 20220801222349.0 | ||
007 | cr nn 008mamaa | ||
008 | 161209s2017 sz | s |||| 0|eng d | ||
020 |
_a9783319460550 _9978-3-319-46055-0 |
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024 | 7 |
_a10.1007/978-3-319-46055-0 _2doi |
|
050 | 4 | _aTL1-4050 | |
072 | 7 |
_aTRP _2bicssc |
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_aTTDS _2bicssc |
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_aTRP _2thema |
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_a629.1 _223 |
100 | 1 |
_aDirkx, Dominic. _eauthor. _4aut _4http://id.loc.gov/vocabulary/relators/aut _961093 |
|
245 | 1 | 0 |
_aConceptual Shape Optimization of Entry Vehicles _h[electronic resource] : _bApplied to Capsules and Winged Fuselage Vehicles / _cby Dominic Dirkx, Erwin Mooij. |
250 | _a1st ed. 2017. | ||
264 | 1 |
_aCham : _bSpringer International Publishing : _bImprint: Springer, _c2017. |
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300 |
_aXVI, 280 p. 178 illus., 130 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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490 | 1 |
_aSpringer Aerospace Technology, _x1869-1749 |
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505 | 0 | _aIntroduction -- Mission Heritage -- Flight Mechanics -- Aerothermodynamics -- Numerical Interpolation -- Vehicle Geometry -- Optimization -- Simulator Development -- Results - Capsule -- Results - Winged Vehicle -- Concluding Remarks. | |
520 | _aThis book covers the parameterization of entry capsules, including Apollo capsules and planetary probes, and winged entry vehicles such as the Space Shuttle and lifting bodies. The aerodynamic modelling is based on a variety of panel methods that take shadowing into account, and it has been validated with flight and wind tunnel data of Apollo and the Space Shuttle. The shape optimization is combined with constrained trajectory analysis, and the multi-objective approach provides the engineer with a Pareto front of optimal shapes. The method detailed in Conceptual Shape Optimization of Entry Vehicles is straightforward, and the output gives the engineer insight in the effect of shape variations on trajectory performance. All applied models and algorithms used are explained in detail, allowing for reconstructing the design tool to the researcher’s requirements. Conceptual Shape Optimization of Entry Vehicles will be of interest to both researchers and graduate students in the field of aerospace engineering, and to practitioners within the aerospace industry. | ||
650 | 0 |
_aAerospace engineering. _96033 |
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650 | 0 |
_aAstronautics. _961094 |
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650 | 0 |
_aThermodynamics. _93554 |
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650 | 1 | 4 |
_aAerospace Technology and Astronautics. _961095 |
650 | 2 | 4 |
_aThermodynamics. _93554 |
700 | 1 |
_aMooij, Erwin. _eauthor. _4aut _4http://id.loc.gov/vocabulary/relators/aut _961096 |
|
710 | 2 |
_aSpringerLink (Online service) _961097 |
|
773 | 0 | _tSpringer Nature eBook | |
776 | 0 | 8 |
_iPrinted edition: _z9783319460543 |
776 | 0 | 8 |
_iPrinted edition: _z9783319460567 |
776 | 0 | 8 |
_iPrinted edition: _z9783319834306 |
830 | 0 |
_aSpringer Aerospace Technology, _x1869-1749 _961098 |
|
856 | 4 | 0 | _uhttps://doi.org/10.1007/978-3-319-46055-0 |
912 | _aZDB-2-ENG | ||
912 | _aZDB-2-SXE | ||
942 | _cEBK | ||
999 |
_c80688 _d80688 |