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Airbreathing Hypersonic Propulsion, Bruno


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Автор: Bruno
Название:  Airbreathing Hypersonic Propulsion
ISBN: 9789811979262
Издательство: Springer
Классификация:


ISBN-10: 981197926X
Обложка/Формат: Hardback
Страницы: 278
Вес: 0.00 кг.
Серия: Space Propulsion
Язык: English
Иллюстрации: XLIV, 273 p. 123 illus., 72 illus. in color.
Читательская аудитория: Science
Основная тема: Engineering
Ссылка на Издательство: Link
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Поставляется из: Германии
Описание: This book details science of hypersonics especially focusing on propulsion aspects such as supersonic combustion ramjets and their applications, and also includes lift and drag in hypersonic flight and their mathematical and physical explanation. It provides charts and data from hypersonic testing and measurements from actual vehicles and engines built in the past. Criteria to dimension hypersonic powered and unpowered vehicles (gliders) based on fundamental fluid dynamics and backed by flight testing; criteria to preliminary sizing vehicles and preliminary dimensioning of supersonic combustors are introduced. The book will serve better theoretical understanding of drag, lift and how to apply them to the design of hypersonic vehicles, as well as data to size vehicles and supersonic combustion ramjet (SCRJ) systems. This book will be a useful reference for researchers and designers in hypersonic vehicles but also second or third-year graduate students.
Дополнительное описание: Why Hypersonic Propulsion?.- Some Aero-Thermodynamics.- Propulsion Cycles.- Hypersonic Flight and its Impact on Propulsion.- Turbulence and Mixing.- Combustion.- Hypersonic Flow Simulation.


Advances in Hypersonics

Автор: BALLMANN; BERTIN; PERIAUX
Название: Advances in Hypersonics
ISBN: 1461267293 ISBN-13(EAN): 9781461267294
Издательство: Springer
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Цена: 46570.00 T
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Reaching High Altitudes on Mars With an Inflatable Hypersonic Drag Balloon

Автор: Hannes Stephan Griebel
Название: Reaching High Altitudes on Mars With an Inflatable Hypersonic Drag Balloon
ISBN: 3834814253 ISBN-13(EAN): 9783834814258
Издательство: Springer
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Цена: 95770.00 T
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Описание: Tbe main purpose of this work was to find a way of placing a meaningful scientific payload within the upper atmosphere of Mars such that certain scientific measurements become possible. So the altitude range covered and the possible dweIl time are relevant design drivers and will be explored in greater detail within this thesis. Either concept of flying on Mars, however, be it heavier or lighter than air (read: heavier or lighter than carbon dioxide) is restricted to altitodes weil below 10 km. Since any sustained light at that altitode or higher in such a thin atmosphere is teehnically impractical, so is ascending to that altitode with - sounding rocket. Therefore - team of scientists from several research institutes around Europe fonned a scientific committec. Together with engineers and scientists from tbe Mars Society Germany and tbe University ofthe Federal Armed Forces of Germany in Munich (UBW) the committee drafted a reference scientific mission scenario 1] to: find ways to da exactly that: providing an instrument suite with access to a large altitu. de range and. meaningful dwell time (see 10. 3. 1 starting onp. ge 208). Tbc most practical approach was found in an inflatable entry vehicle that can provide the largest and lightest possible configuration. Since 00 such attempts have yet been m. ade, the work described herein focuses mostly on the mathematical thcory and the technical peculiarities of such a system, but also treats mission design and testing aspects. 1.

Advances in Hypersonics

Автор: Bertin; Ballmann; Periaux
Название: Advances in Hypersonics
ISBN: 1461267307 ISBN-13(EAN): 9781461267300
Издательство: Springer
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Цена: 46570.00 T
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Hypersonics

Автор: BERTIN; GLOWINSKI; PERIAUX
Название: Hypersonics
ISBN: 146849189X ISBN-13(EAN): 9781468491890
Издательство: Springer
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Цена: 46570.00 T
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Описание: Configurations that have a relatively high ballistic coefficient (such as slender reentry vehicles) and reenter the atmosphere at relatively high angles of attack experience severe heating rates and high dynamic pressures, but only for a short period of time.

Airbreathing Propulsion

Автор: Tarit Bose
Название: Airbreathing Propulsion
ISBN: 149390180X ISBN-13(EAN): 9781493901807
Издательство: Springer
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Цена: 65290.00 T
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Описание: This unified approach to teaching the physics of combustion, fluid dynamics and other properties of aircraft engines covers both modern and historical power units and features exercises and extensive data that allow readers to evaluate comparative results.

Prediction and Validation Technologies of Aerodynamic Force and Heat for Hypersonic Vehicle Design

Автор: Zhao Min
Название: Prediction and Validation Technologies of Aerodynamic Force and Heat for Hypersonic Vehicle Design
ISBN: 9813365250 ISBN-13(EAN): 9789813365254
Издательство: Springer
Цена: 167700.00 T
Наличие на складе: Есть у поставщика Поставка под заказ.
Описание: Given its scope, the book offers a valuable asset for researchers who are interested in thermodynamics, aircraft design, wind tunnel testing, fluid dynamics and aerothermodynamics research methods, introducing them to inspiring new research topics.

Steady Glide Dynamics and Guidance of Hypersonic Vehicle

Автор: Chen Wanchun, Zhou Hao, Yu Wenbin
Название: Steady Glide Dynamics and Guidance of Hypersonic Vehicle
ISBN: 9811589038 ISBN-13(EAN): 9789811589034
Издательство: Springer
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Цена: 149060.00 T
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Описание: Introduction.- Mathematical Fundamentals.- The Mathematical Model for Hypersonic Entry Glide Vehicle.- Mathematical description of optimal control problem for entry gliding.- Indirect approch to the optimal glide trajectory problem.- Direct Method for Gliding Trajectory Optimization Problem.- The Concept of Steady Glide Reentry Trajectory and the Stability of its Regular Perturbation Solutions.- Analytical Solutions of Steady Glide Reentry Trajectory in Three Dimensions and their Application to Trajectory Planning.- Trajectory Damping Control Technique for Hypersonic Glide Reentry.- Steady Glide Dynamic Modeling and Trajectory Optimization for High Lift-to-Drag Ratio Reentry Vehicle.- Singular Perturbation Guidance of Hypersonic Glide Reentry.- 3-D Reentry Guidance with Real-Time Planning of Reference with New Analytical Solutions Based on Spectral Decomposition Method.- Omnidirectional Autonomous Reentry Guidance Based on 3-D Analytical glide Formulas with the Consideration of the effects of the Earth's rotation.- Analytical Entry Guidance based on Steady Glide.- Linear Pseudospectral General Nominal Effort Miss Distance Guidance Method.- Linear Pseudospectral Adaptive Flight Phase Segmentation General Nominal Effort Miss Distance Reentry Guidance.- Trajectory-Shaping Guidance with Final Speed and Load Factor Constraints.

Classic and high-enthalpy hypersonic flows

Автор: Shang, Joseph J.s. (wright State University, Usa)
Название: Classic and high-enthalpy hypersonic flows
ISBN: 1032079819 ISBN-13(EAN): 9781032079813
Издательство: Taylor&Francis
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Цена: 102080.00 T
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Computational Methods in Hypersonic Aerodynamics

Автор: T.K.S. Murthy
Название: Computational Methods in Hypersonic Aerodynamics
ISBN: 0792316738 ISBN-13(EAN): 9780792316732
Издательство: Springer
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Цена: 261210.00 T
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Описание: Contains chapters on computational methods in hypersonic aerodynamics. This book includes the effects of viscosity on the physical and chemical processes of high-temperature nonequilibrium flow at very high speeds, such as vibrational excitation, dissociation and recombination, and ionization and radiation.

Super- and Hypersonic Aerodynamics and Heat Transfer

Автор: Parton, V.Z.
Название: Super- and Hypersonic Aerodynamics and Heat Transfer
ISBN: 0849393094 ISBN-13(EAN): 9780849393099
Издательство: Taylor&Francis
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Цена: 137810.00 T
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US Hypersonic Research and Development: The Rise and Fall of `Dyna-Soar`, 1944-1963

Автор: Roy F. Houchin II
Название: US Hypersonic Research and Development: The Rise and Fall of `Dyna-Soar`, 1944-1963
ISBN: 0415654718 ISBN-13(EAN): 9780415654715
Издательство: Taylor&Francis
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Цена: 57150.00 T
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Описание: This is a history of the US military`s `Dyna-Soar` project to build a hypersonic reusable `space plane`, which lasted from 1945 to 1963.

Steady Glide Dynamics and Guidance of Hypersonic Vehicle

Автор: Chen Wanchun, Zhou Hao, Yu Wenbin
Название: Steady Glide Dynamics and Guidance of Hypersonic Vehicle
ISBN: 9811589003 ISBN-13(EAN): 9789811589003
Издательство: Springer
Цена: 149060.00 T
Наличие на складе: Есть у поставщика Поставка под заказ.
Описание: Introduction.- Mathematical Fundamentals.- The Mathematical Model for Hypersonic Entry Glide Vehicle.- Mathematical description of optimal control problem for entry gliding.- Indirect approch to the optimal glide trajectory problem.- Direct Method for Gliding Trajectory Optimization Problem.- The Concept of Steady Glide Reentry Trajectory and the Stability of its Regular Perturbation Solutions.- Analytical Solutions of Steady Glide Reentry Trajectory in Three Dimensions and their Application to Trajectory Planning.- Trajectory Damping Control Technique for Hypersonic Glide Reentry.- Steady Glide Dynamic Modeling and Trajectory Optimization for High Lift-to-Drag Ratio Reentry Vehicle.- Singular Perturbation Guidance of Hypersonic Glide Reentry.- 3-D Reentry Guidance with Real-Time Planning of Reference with New Analytical Solutions Based on Spectral Decomposition Method.- Omnidirectional Autonomous Reentry Guidance Based on 3-D Analytical glide Formulas with the Consideration of the effects of the Earth's rotation.- Analytical Entry Guidance based on Steady Glide.- Linear Pseudospectral General Nominal Effort Miss Distance Guidance Method.- Linear Pseudospectral Adaptive Flight Phase Segmentation General Nominal Effort Miss Distance Reentry Guidance.- Trajectory-Shaping Guidance with Final Speed and Load Factor Constraints.


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