Conceptual Shape Optimization of Entry Vehicles (Record no. 80688)
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| 000 -LEADER | |
|---|---|
| fixed length control field | 03384nam a22005655i 4500 |
| 001 - CONTROL NUMBER | |
| control field | 978-3-319-46055-0 |
| 005 - DATE AND TIME OF LATEST TRANSACTION | |
| control field | 20220801222349.0 |
| 008 - FIXED-LENGTH DATA ELEMENTS--GENERAL INFORMATION | |
| fixed length control field | 161209s2017 sz | s |||| 0|eng d |
| 020 ## - INTERNATIONAL STANDARD BOOK NUMBER | |
| ISBN | 9783319460550 |
| -- | 978-3-319-46055-0 |
| 082 04 - CLASSIFICATION NUMBER | |
| Call Number | 629.1 |
| 100 1# - AUTHOR NAME | |
| Author | Dirkx, Dominic. |
| 245 10 - TITLE STATEMENT | |
| Title | Conceptual Shape Optimization of Entry Vehicles |
| Sub Title | Applied to Capsules and Winged Fuselage Vehicles / |
| 250 ## - EDITION STATEMENT | |
| Edition statement | 1st ed. 2017. |
| 300 ## - PHYSICAL DESCRIPTION | |
| Number of Pages | XVI, 280 p. 178 illus., 130 illus. in color. |
| 490 1# - SERIES STATEMENT | |
| Series statement | Springer Aerospace Technology, |
| 505 0# - FORMATTED CONTENTS NOTE | |
| Remark 2 | Introduction -- Mission Heritage -- Flight Mechanics -- Aerothermodynamics -- Numerical Interpolation -- Vehicle Geometry -- Optimization -- Simulator Development -- Results - Capsule -- Results - Winged Vehicle -- Concluding Remarks. |
| 520 ## - SUMMARY, ETC. | |
| Summary, etc | 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 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. |
| 700 1# - AUTHOR 2 | |
| Author 2 | Mooij, Erwin. |
| 856 40 - ELECTRONIC LOCATION AND ACCESS | |
| Uniform Resource Identifier | https://doi.org/10.1007/978-3-319-46055-0 |
| 942 ## - ADDED ENTRY ELEMENTS (KOHA) | |
| Koha item type | eBooks |
| 264 #1 - | |
| -- | Cham : |
| -- | Springer International Publishing : |
| -- | Imprint: Springer, |
| -- | 2017. |
| 336 ## - | |
| -- | text |
| -- | txt |
| -- | rdacontent |
| 337 ## - | |
| -- | computer |
| -- | c |
| -- | rdamedia |
| 338 ## - | |
| -- | online resource |
| -- | cr |
| -- | rdacarrier |
| 347 ## - | |
| -- | text file |
| -- | |
| -- | rda |
| 650 #0 - SUBJECT ADDED ENTRY--SUBJECT 1 | |
| -- | Aerospace engineering. |
| 650 #0 - SUBJECT ADDED ENTRY--SUBJECT 1 | |
| -- | Astronautics. |
| 650 #0 - SUBJECT ADDED ENTRY--SUBJECT 1 | |
| -- | Thermodynamics. |
| 650 14 - SUBJECT ADDED ENTRY--SUBJECT 1 | |
| -- | Aerospace Technology and Astronautics. |
| 650 24 - SUBJECT ADDED ENTRY--SUBJECT 1 | |
| -- | Thermodynamics. |
| 830 #0 - SERIES ADDED ENTRY--UNIFORM TITLE | |
| -- | 1869-1749 |
| 912 ## - | |
| -- | ZDB-2-ENG |
| 912 ## - | |
| -- | ZDB-2-SXE |
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