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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
024 7 _a10.1007/978-3-319-46055-0
_2doi
050 4 _aTL1-4050
072 7 _aTRP
_2bicssc
072 7 _aTTDS
_2bicssc
072 7 _aTEC002000
_2bisacsh
072 7 _aTRP
_2thema
072 7 _aTTDS
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082 0 4 _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.
300 _aXVI, 280 p. 178 illus., 130 illus. in color.
_bonline resource.
336 _atext
_btxt
_2rdacontent
337 _acomputer
_bc
_2rdamedia
338 _aonline resource
_bcr
_2rdacarrier
347 _atext file
_bPDF
_2rda
490 1 _aSpringer Aerospace Technology,
_x1869-1749
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
650 0 _aAstronautics.
_961094
650 0 _aThermodynamics.
_93554
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