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000698074 020__ $$a9783642541681 $$qelectronic book
000698074 020__ $$a3642541682 $$qelectronic book
000698074 020__ $$z9783642541674
000698074 0247_ $$a10.1007/978-3-642-54168-1$$2doi
000698074 035__ $$aSP(OCoLC)ocn879182351
000698074 035__ $$aSP(OCoLC)879182351
000698074 040__ $$aGW5XE$$beng$$erda$$epn$$cGW5XE$$dCOO
000698074 049__ $$aISEA
000698074 050_4 $$aTL1050
000698074 08204 $$a629.4/151$$223
000698074 1001_ $$aWeiland, Claus,$$eauthor.
000698074 24510 $$aAerodynamic data of space vehicles$$h[electronic resource]  /$$cClaus Weiland.
000698074 264_1 $$aHeidelberg :$$bSpringer,$$c2014.
000698074 300__ $$a1 online resource (xvi, 355 pages) :$$billustrations (some color)
000698074 336__ $$atext$$btxt$$2rdacontent
000698074 337__ $$acomputer$$bc$$2rdamedia
000698074 338__ $$aonline resource$$bcr$$2rdacarrier
000698074 504__ $$aIncludes bibliographical references and indexes.
000698074 506__ $$aAccess limited to authorized users.
000698074 520__ $$aThe capacity and quality of the atmospheric flight performance of space flight vehicles is characterized by their aerodynamic data bases. A complete aerodynamic data base would encompass the coefficients of the static longitudinal and lateral motions and the related dynamic coefficients. In this book the aerodynamics of 27 vehicles are considered. Only a few of them did really fly. Therefore the aerodynamic data bases are often not complete, in particular when the projects or programs were more or less abruptly stopped, often due to political decisions. Configurational design studies or the development of demonstrators usually happen with reduced or incomplete aerodynamic data sets. Therefore some data sets base just on the application of one of the following tools: semi-empirical design methods, wind tunnel tests, numerical simulations. In so far a high percentage of the data presented is incomplete and would have to be verified. Flight mechanics needs the aerodynamic coefficients as function of a lot of variables. The allocation of the aerodynamic coefficients for a particular flight operation at a specific trajectory point is conducted by an aerodynamic model. The establishment of such models is described in this book. This book is written for graduate and doctoral students to give them insight into the aerodynamics of the various flight configurations. Further for design and development engineers in industry and at research institutes (including universities) searching for an appropriate vehicle shape, as well as for non-specialists, who may be interested in this subject. The book will be helpful, too, in the case that system studies require in their concept phases the selection of suitable vehicle shapes.
000698074 588__ $$aDescription based on online resource; title from PDF title page (SpringerLink, viewed May 5, 2014).
000698074 650_0 $$aSpace vehicles$$xAerodynamics.
000698074 852__ $$bebk
000698074 85640 $$3SpringerLink$$uhttps://univsouthin.idm.oclc.org/login?url=http://dx.doi.org/10.1007/978-3-642-54168-1$$zOnline Access
000698074 909CO $$ooai:library.usi.edu:698074$$pGLOBAL_SET
000698074 980__ $$aEBOOK
000698074 980__ $$aBIB
000698074 982__ $$aEbook
000698074 983__ $$aOnline
000698074 994__ $$a92$$bISE