Aerodynamic Data of Space Vehicles (Record no. 54800)

000 -LEADER
fixed length control field 03675nam a22005295i 4500
001 - CONTROL NUMBER
control field 978-3-642-54168-1
005 - DATE AND TIME OF LATEST TRANSACTION
control field 20200421111658.0
008 - FIXED-LENGTH DATA ELEMENTS--GENERAL INFORMATION
fixed length control field 140222s2014 gw | s |||| 0|eng d
020 ## - INTERNATIONAL STANDARD BOOK NUMBER
ISBN 9783642541681
-- 978-3-642-54168-1
082 04 - CLASSIFICATION NUMBER
Call Number 629.1
100 1# - AUTHOR NAME
Author Weiland, Claus.
245 10 - TITLE STATEMENT
Title Aerodynamic Data of Space Vehicles
300 ## - PHYSICAL DESCRIPTION
Number of Pages XVI, 355 p. 403 illus., 269 illus. in color.
505 0# - FORMATTED CONTENTS NOTE
Remark 2 The Discipline Aerodynamics -- Classi�cation and Comprehension of Space Vehicles -- Aerothermodynamic Data of Non-winged Re-entry Vehicles (RV-NW)Capsules and Probes -- Erothermodynamic Data of Non-winged Re-entry Vehicles (RV-NW) -- Cones and Bicones.
520 ## - SUMMARY, ETC.
Summary, etc The capacity and quality of the atmospheric flight performance of space flight vehicles is characterized by their aerodynamic data bases. A complete aerodynamic data base would encompass the coefficients of the static longitudinal and lateral motions and the related dynamic coefficients. In this book the aerodynamics of 27 vehicles are considered. Only a few of them did really fly. Therefore the aerodynamic data bases are often not complete, in particular when the projects or programs were more or less abruptly stopped, often due to political decisions. Configurational design studies or the development of demonstrators usually happen with reduced or incomplete aerodynamic data sets. Therefore some data sets base just on the application of one of the following tools: semi-empirical design methods, wind tunnel tests, numerical simulations. In so far a high percentage of the data presented is incomplete and would have to be verified. Flight mechanics needs the aerodynamic coefficients as function of a lot of variables. The allocation of the aerodynamic coefficients for a particular flight operation at a specific trajectory point is conducted by an aerodynamic model. The establishment of such models is described in this book. This book is written for graduate and doctoral students to give them insight into the aerodynamics of the various flight configurations. Further for design and development engineers in industry and at research institutes (including universities) searching for an appropriate vehicle shape, as well as for non-specialists, who may be interested in this subject. The book will be helpful, too, in the case that system studies require in their concept phases the selection of suitable vehicle shapes.
856 40 - ELECTRONIC LOCATION AND ACCESS
Uniform Resource Identifier http://dx.doi.org/10.1007/978-3-642-54168-1
942 ## - ADDED ENTRY ELEMENTS (KOHA)
Koha item type eBooks
264 #1 -
-- Berlin, Heidelberg :
-- Springer Berlin Heidelberg :
-- Imprint: Springer,
-- 2014.
336 ## -
-- text
-- txt
-- rdacontent
337 ## -
-- computer
-- c
-- rdamedia
338 ## -
-- online resource
-- cr
-- rdacarrier
347 ## -
-- text file
-- PDF
-- rda
650 #0 - SUBJECT ADDED ENTRY--SUBJECT 1
-- Engineering.
650 #0 - SUBJECT ADDED ENTRY--SUBJECT 1
-- Fluids.
650 #0 - SUBJECT ADDED ENTRY--SUBJECT 1
-- Thermodynamics.
650 #0 - SUBJECT ADDED ENTRY--SUBJECT 1
-- Heat engineering.
650 #0 - SUBJECT ADDED ENTRY--SUBJECT 1
-- Heat transfer.
650 #0 - SUBJECT ADDED ENTRY--SUBJECT 1
-- Mass transfer.
650 #0 - SUBJECT ADDED ENTRY--SUBJECT 1
-- Aerospace engineering.
650 #0 - SUBJECT ADDED ENTRY--SUBJECT 1
-- Astronautics.
650 14 - SUBJECT ADDED ENTRY--SUBJECT 1
-- Engineering.
650 24 - SUBJECT ADDED ENTRY--SUBJECT 1
-- Aerospace Technology and Astronautics.
650 24 - SUBJECT ADDED ENTRY--SUBJECT 1
-- Fluid- and Aerodynamics.
650 24 - SUBJECT ADDED ENTRY--SUBJECT 1
-- Engineering Thermodynamics, Heat and Mass Transfer.
912 ## -
-- ZDB-2-ENG

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