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Super- and Hypersonic Aerodynamics and Heat Transfer, Parton, V.Z.


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Автор: Parton, V.Z.
Название:  Super- and Hypersonic Aerodynamics and Heat Transfer
ISBN: 9780849393099
Издательство: Taylor&Francis
Классификация:

ISBN-10: 0849393094
Обложка/Формат: Hardback
Страницы: 352
Вес: 0.66 кг.
Дата издания: 10.11.1992
Язык: English
Иллюстрации: 2 tables, black and white
Размер: 240 x 163 x 24
Читательская аудитория: Undergraduate
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Поставляется из: Европейский союз


Fundamentals Of Aerodynamics

Автор: Anderson
Название: Fundamentals Of Aerodynamics
ISBN: 1259251349 ISBN-13(EAN): 9781259251344
Издательство: McGraw-Hill
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Цена: 10123.00 р.
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Описание: In this richly illustrated book, Robert Macieski examines Lewis W. Hine`s art and advocacy on behalf of child labourers as part of the National Child Labor Committee (NCLC) between 1909 and 1917. A "social photographer", Hine created images that documented children at work throughout New England, making the case for their exploitation in the North as he had for rural working children in the South.

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: 14365.00 р.
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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.

Hypersonic Curved Compression Inlet and Its Inverse Design

Автор: Zhang Kunyuan
Название: Hypersonic Curved Compression Inlet and Its Inverse Design
ISBN: 9811507260 ISBN-13(EAN): 9789811507267
Издательство: Springer
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Цена: 30745.00 р.
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Описание: This book presents systematic research results on curved shock wave-curved compression surface applied to the compression surface design of supersonic-hypersonic inlet, which is a brand new inlet design.

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: 39182.00 р.
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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.

Hypersonics

Автор: BERTIN; GLOWINSKI; PERIAUX
Название: Hypersonics
ISBN: 146849189X ISBN-13(EAN): 9781468491890
Издательство: Springer
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Цена: 6986.00 р.
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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.

Advances in Hypersonics

Автор: BALLMANN; BERTIN; PERIAUX
Название: Advances in Hypersonics
ISBN: 1461267293 ISBN-13(EAN): 9781461267294
Издательство: Springer
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Цена: 6986.00 р.
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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: 25155.00 р.
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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.

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: 9813365285 ISBN-13(EAN): 9789813365285
Издательство: Springer
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Цена: 25155.00 р.
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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.

Applied Computational Aerodynamics

Автор: Cummings
Название: Applied Computational Aerodynamics
ISBN: 1107053749 ISBN-13(EAN): 9781107053748
Издательство: Cambridge Academ
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Цена: 16474.00 р.
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Описание: This computational aerodynamics (CA) textbook is written at the undergraduate level and focuses on developing the engineering skills required to become an intelligent user of aerodynamic simulation codes. This is done by taking advantage of CA codes that are now available and doing projects to learn the basic numerical and aerodynamic concepts.

Thermal Protection Modeling of Hypersonic Flying Apparatus

Автор: Yakimov
Название: Thermal Protection Modeling of Hypersonic Flying Apparatus
ISBN: 3319782169 ISBN-13(EAN): 9783319782164
Издательство: Springer
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Цена: 19564.00 р.
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Описание: This book is devoted to studies of unsteady heat and mass exchange processes taking into account thermochemical destruction of thermal protective materials, research of transpiration cooling systems, thermal protection of composite materials exposed to low-energy disturbances, as well as the numerical solution of heat and mass transfer of the exchange. It proposes several mathematical models of passive and active thermal protection systems with regard to factors such as surface ablation, surface roughness, phase transition of a liquid in porous materials, rotation of the body around its longitudinal axis, and exposure to low-energy disturbances. The author studies the possibilities to control thermochemical destruction and heat mass exchange processes in transpiration cooling systems exposed to low-energy disturbances. The numerical analysis of the heat and mass exchange process in carbon plastics under repeated impulse action is also presented. The numerical solutions of problems are compared with the known experimental data. The book is intended for specialists in the field of thermal protection and heat mass exchange, as well as graduate and undergraduates in physics and mathematics.

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: 22359.00 р.
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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: 15312.00 р.
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