東華大學圖書館 |

語系: 繁體中文

說明(常見問題)

回圖書館首頁

手機版館藏查詢

登入

回首頁

切換: 標籤 | MARC模式 | ISBD

Conceptual shape optimization of ent...

Dirkx, Dominic.

FindBook

Google Book

Amazon

博客來

Conceptual shape optimization of entry vehicles = applied to capsules and winged fuselage vehicles /

紀錄類型:	書目-電子資源 : Monograph/item
正題名/作者:	Conceptual shape optimization of entry vehicles/ by Dominic Dirkx, Erwin Mooij.
其他題名:	applied to capsules and winged fuselage vehicles /
作者:	Dirkx, Dominic.
其他作者:	Mooij, Erwin.
出版者:	Cham :Springer International Publishing : : 2017.,
面頁冊數:	xvi, 280 p. :ill., digital ;24 cm.
內容註:	Introduction -- Mission Heritage -- Flight Mechanics -- Aerothermodynamics -- Numerical Interpolation -- Vehicle Geometry -- Optimization -- Simulator Development -- Results - Capsule -- Results - Winged Vehicle -- Concluding Remarks.
Contained By:	Springer eBooks
標題:	Space vehicles - Atmospheric entry. -
電子資源:	http://dx.doi.org/10.1007/978-3-319-46055-0
ISBN:	9783319460550

Conceptual shape optimization of entry vehicles = applied to capsules and winged fuselage vehicles /
Dirkx, Dominic.

Conceptual shape optimization of entry vehiclesapplied to capsules and winged fuselage vehicles /[electronic resource] :by Dominic Dirkx, Erwin Mooij. - Cham :Springer International Publishing :2017. - xvi, 280 p. :ill., digital ;24 cm. - Springer aerospace technology,1869-1730. - Springer aerospace technology..

Introduction -- Mission Heritage -- Flight Mechanics -- Aerothermodynamics -- Numerical Interpolation -- Vehicle Geometry -- Optimization -- Simulator Development -- Results - Capsule -- Results - Winged Vehicle -- Concluding Remarks.

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.

ISBN: 9783319460550

Standard No.: 10.1007/978-3-319-46055-0doiSubjects--Topical Terms:

3219530
Space vehicles
--Atmospheric entry.

LC Class. No.: TL1060

Dewey Class. No.: 629.4588

Conceptual shape optimization of entry vehicles = applied to capsules and winged fuselage vehicles /
LDR:02369nmm a2200337 a 4500 001 2089163
003 DE-He213
005 20170628112609.0
006 m d
007 cr nn 008maaau
008 171013s2017 gw s 0 eng d
020 $a 9783319460550 $q (electronic bk.)
020 $a 9783319460543 $q (paper)
024 7 $a 10.1007/978-3-319-46055-0 $2 doi
035 $a 978-3-319-46055-0
040 $a GP $c GP
041 0 $a eng
050 4 $a TL1060
072 7 $a TRP $2 bicssc
072 7 $a TTDS $2 bicssc
072 7 $a TEC002000 $2 bisacsh
082 0 4 $a 629.4588 $2 23
090 $a TL1060 $b .D599 2017
100 1 $a Dirkx, Dominic. $3 3219528
245 1 0 $a Conceptual shape optimization of entry vehicles $h [electronic resource] : $b applied to capsules and winged fuselage vehicles / $c by Dominic Dirkx, Erwin Mooij.
260 $a Cham : $b Springer International Publishing : $b Imprint: Springer, $c 2017.
300 $a xvi, 280 p. : $b ill., digital ; $c 24 cm.
490 1 $a Springer aerospace technology, $x 1869-1730
505 0 $a Introduction -- Mission Heritage -- Flight Mechanics -- Aerothermodynamics -- Numerical Interpolation -- Vehicle Geometry -- Optimization -- Simulator Development -- Results - Capsule -- Results - Winged Vehicle -- Concluding Remarks.
520 $a 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.
650 0 $a Space vehicles $x Atmospheric entry. $3 3219530
650 1 4 $a Engineering. $3 586835
650 2 4 $a Aerospace Technology and Astronautics. $3 928116
650 2 4 $a Thermodynamics. $3 517304
700 1 $a Mooij, Erwin. $3 3219529
710 2 $a SpringerLink (Online service) $3 836513
773 0 $t Springer eBooks
830 0 $a Springer aerospace technology. $3 1566537
856 4 0 $u http://dx.doi.org/10.1007/978-3-319-46055-0
950 $a Engineering (Springer-11647)