This book presents the historical overview of the development of the reusable hypersonic aircraft systems. Methods to predict aerothermodynamic characteristics for hypersonic aircrafts and application of cognitive approach in computational aerodynamics are offered. The basic principles of hypersonic propulsion systems: rocket engines, turbofan, turbojet, ramjet, scramjet and the dual-combustion ramjet are explained. The book also highlighted that we need to consider medico-biological effect and to improve biological and medical system for human in space flight due to future space exploration plans to deliver manned spacecrafts with crews to the Moon and Mars.
The Full Book PDF |
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Front Matter |
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Chapter 1 Introduction |
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1.1 Historical Overview
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1.2 The Russian Aerospace Programs
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1.2.1 The Clipper
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1.2.2 The Rus
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1.2.3 The Baikal
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1.3 Hypersonic Aircraft Programs of the United States
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1.3.1 The X-51
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1.3.2 The FALCON Project
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1.3.3 The XS-1
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1.3.4 The SR-72
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1.4 Europe’s Ambition for Spacecrafts
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1.5 Aerospace Programs of Other Developed Countries
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Chapter 2 Monte-Carlo Methods in High-Altitude Aerodynamics |
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2.1 Basic Principle of Monte-Carlo Methods
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2.2 The Monte Carlo Methods in Computational Aerodynamics
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2.3 Method for Surface Description of the Complex Vehicle Design
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2.4 The Mathematical Description of Gas-Surface Interaction Models
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2.4.1 Maxwell Model
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2.4.2 Cercignani-Lampis-Lord Model
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2.4.3 Nocilla Model
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2.4.4 Lennard-Jones Potential
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2.5 Modelling of the Aerodynamic Characteristics of Aerospace Vehicles in Free Molecular Flow
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Chapter 3 Methods for Determining Aerothermodynamic Characteristics of High-Speed Aircraft Vehicles in Transitional Flow Regime |
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3.1 Local Engineering Methods
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3.2 Local-Bridging Method to Predict Aerothermodynamic Characteristics of High-Speed Aircraft Vehicles in the Transitional Regime
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3.3 Methods to Calculate Heat Transfer Coefficients in Boundary Layer
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3.3.1 Formulas for Calculating Heat Transfer in Laminar Boundary Layer
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3.3.2 Formulas for Calculating Heat Transfer in Turbulent Boundary Layer
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Chapter 4 Application of Cognitive Technology in Computational Aerodynamics |
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4.1 Development of Cognitive Technology in Modern Sciences
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4.2 Application of Artificial Neural Networks in Hypersonic Aerospace Technology
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4.2.1 Principle of Biological Neural Networks
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4.2.2 Principle of Artificial Neural Networks
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4.3 The Training on Artificial Neural Networks for Aerodynamic Characteristics of Hypersonic Vehicle
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Chapter 5 Basic Concepts of Propulsion System for High-Speed Aircrafts |
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5.1 Rocket Engines
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5.2 Turbojet
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5.3 Turbofan
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5.4 Airbreathing Propulsion Systems for High-Speed Aircraft Vehicles
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5.5 Ramjet
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5.6 Scramjet
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5.7 Dual Combustion Ramjet and Dual Mode Ramjet
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Chapter 6 A Future Space Transportation System |
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6.1 Space Elevator
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6.2 Medical and Biological Aspects in Human Spaceflight
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6.3 Advances of Space Medicine and Biology Research
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Back Matter |
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Yuri Ivanovich Khlopkov
Doctor of Physical and Mathematical Sciences, Leading Researcher, Central Aerohydrodynamic Institute named after professor N.E. Zhukovsky, Russia; Professor, Moscow Institute of Physics and Technology (State University), Russia; Academician of the Russian Academy of Natural History.
Sergey Leonidovich Chernyshev
Doctor of Physical and Mathematical Sciences; General Director, Central Aerohydrodynamic Institute named after Professor N.E. Zhukovsky, Russia; Professor, Moscow Institute of Physics and Technology (State University), Russia; Corresponding Member of Russian Academy of Sciences.
Zay Yar Myo Myint
Candidate of Physical and Mathematical Sciences; Doctoral Candidate, Moscow Institute of Physics and Technology (State University), Russia; Professor of Russian Academy of Natural History.
Anton Yurievich Khlopkov
Programming Engineer, Moscow Institute of Physics and Technology (State University), Russia.
Alena Anatolevna Sorokina
M.Sc. student, Moscow Institute of Physics and Technology (State University), Russia.
This book is more suitable for students, specialists, scientific researchers and the readers who are interesting in high-speed aircraft engineering and aerospace technology.