[PDF.02sl] Conceptual Shape Optimization of Entry Vehicles: Applied to Capsules and Winged Fuselage Vehicles (Springer Aerospace Technology)
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Conceptual Shape Optimization of Entry Vehicles: Applied to Capsules and Winged Fuselage Vehicles (Springer Aerospace Technology)
Dominic Dirkx, Erwin Mooij
[PDF.sr87] Conceptual Shape Optimization of Entry Vehicles: Applied to Capsules and Winged Fuselage Vehicles (Springer Aerospace Technology)
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| #4904495 in Books | Erwin Mooij Dominic Dirkx | 2016-12-10 | Original language:English | PDF # 1 | 9.21 x.69 x6.14l,.0 | File type: PDF | 280 pages | Conceptual Shape Optimization of Entry Vehicles Applied to Capsules and Winged Fuselage Vehicles Springer Aerospace Technology||From the Back Cover||This 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
This 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 approac...
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