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

Record Type:	Language materials, printed : Monograph/item
Title/Author:	Conceptual shape optimization of entry vehicles/ by Dominic Dirkx, Erwin Mooij.
Reminder of title:	applied to capsules and winged fuselage vehicles /
Author:	Dirkx, Dominic.
other author:	Mooij, Erwin.
Published:	Cham :Springer International Publishing : : 2017.,
Description:	xvi, 280 p. :ill., digital ; : 24 cm.;
Contained By:	Springer eBooks
Subject:	Space vehicles - Atmospheric entry. -
Online resource:	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:

1249688
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 /
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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.
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