Selected Aerothermodynamic Design Problems of Hypersonic Flight Vehicles

This volume addresses selected aerothermodynamic design problems for three vehicle classes: winged reentry, non-winged reentry, and airbreathing hypersonic flight vehicles. Following an introductory chapter, the book presents the basics of flight trajectory mechanics, giving the aerothermodynamicist...

Cijeli opis

Spremljeno u:
Bibliografski detalji
Glavni autori: Hirschel, Ernst Heinrich, Weiland, Claus (Autor)
Format: Livre numérique
Jezik:Anglais
Izdano: Berlin, Heidelberg : Springer Berlin Heidelberg [20..].
Cham : Springer Nature
Online pristup:Accès sur la plateforme de l'éditeur
Accès sur la plateforme Istex
Accès Université d'Orléans
Accès INSA CVL
Bilješka: Archives Springer e-books (Licence nationale)
Archives Springer e-books (Licence nationale)
Autres localisations: Voir dans le Sudoc
Edition sous un autre format:• Selected aerothermodynamic design problems of hypersonic flight vehicles, Ernst Heinrich Hirschel, Claus Weiland, Berlin, Springer-Verlag, 2009, 1 vol. (XV-518 p.), 978-3-540-89973-0
LEADER 04117nam a22003137a 4500
001 942033
008 100125q2000 xx ||| |||| 00| 0 eng d
009 PPN139961887
020 |a 9783540899747 
041 0 |a eng 
082 |a 629.2 
100 1 |a Hirschel, Ernst Heinrich. 
245 1 0 |a Selected Aerothermodynamic Design Problems of Hypersonic Flight Vehicles   |c by Ernst Heinrich Hirschel, Claus Weiland. 
260 |a Berlin, Heidelberg :  |b Springer Berlin Heidelberg. 
260 |a Cham :  |b Springer Nature,  |c [20..]. 
500 |a Archives Springer e-books (Licence nationale) 
500 |a Archives Springer e-books (Licence nationale) 
505 1 |a Short Introduction to Flight Trajectories for Aerothermodynamicists Aerothermodynamic Design Problems of Winged Re-Entry Vehicles Aerothermodynamic Design Problems of Winged Airbreathing Vehicles Aerothermodynamic Design Problems of Non-Winged Re-Entry Vehicles Stabilization, Trim, and Control Devices Forces, Moments, Center-of-Pressure, Trim, and Stability in General Formulation Multidisciplinary Design Aspects The Thermal State of a Hypersonic Vehicle Surface The ?eff Approach and Approximate Relations for the Determination of Aerothermodynamic Parameters Solution Guide and Solutions of the Problems 
506 |a Accès en ligne pour les établissements français bénéficiaires des licences nationales 
506 |a Accès soumis à abonnement pour tout autre établissement 
506 |a Conditions particulières de réutilisation pour les bénéficiaires des licences nationales. https://www.licencesnationales.fr/springer-nature-ebooks-contrat-licence-ln-2017 
520 |a This volume addresses selected aerothermodynamic design problems for three vehicle classes: winged reentry, non-winged reentry, and airbreathing hypersonic flight vehicles. Following an introductory chapter, the book presents the basics of flight trajectory mechanics, giving the aerothermodynamicist an understanding of the principal issues relevant to the field. In the following chapters, specific aerothermodynamic phenomena are discussed for the three vehicle classes, major simulation problems are singled out, and particular trends are examined. Available coefficients of longitudinal motion are presented for a variety of shapes of operational and studied vehicles, and aerothermodynamic issues of stabilization, trim, and control devices are treated. A full chapter is devoted to describing equations for aerodynamic forces, moments, center of pressure, trim, and stability. Another chapter focuses on multidisciplinary design aspects, presenting the mathematical models and the coupling procedures in detail. Other chapters address the thermal state of a vehicle surface, thermal loads, and thermal surface effects, which are among the major topics of hypersonic vehicle design. The governing equations for flow in thermo-chemical non-equilibrium are presented, along with properties of the earth s atmosphere. Finally, constants and dimensions, symbol definitions, a glossary, acronyms, and a solution guide to problems are provided. This book will be a great boon to graduate students, doctoral students, design and development engineers, and technical managers alike 
700 1 |a Weiland, Claus.  |4 aut 
776 0 |0 147238137  |t Selected aerothermodynamic design problems of hypersonic flight vehicles  |f Ernst Heinrich Hirschel, Claus Weiland  |c Berlin  |n Springer-Verlag  |d 2009  |p 1 vol. (XV-518 p.)  |z 978-3-540-89973-0 
856 4 |q PDF  |u https://doi.org/10.1007/978-3-540-89974-7  |z Accès sur la plateforme de l'éditeur 
856 4 |u https://revue-sommaire.istex.fr/ark:/67375/8Q1-VFQM95CQ-0  |z Accès sur la plateforme Istex 
856 4 |5 452349901:747840709  |u https://ezproxy.univ-orleans.fr/login?url=https://doi.org/10.1007/978-3-540-89974-7  |z Accès Université d'Orléans 
856 4 |5 180339901:750858214  |u https://ezproxy.insa-cvl.fr/login?qurl=https://doi.org/10.1007/978-3-540-89974-7  |z Accès INSA CVL 
997 |0 942033  |1 Livre numérique  |a Ressource numérique  |b INSA  |b ENSA  |c 0/Bibliothèque numérique/  |c 1/Bibliothèque numérique/Autre ressource numérique/