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G. A. Tirskiy S Hypersonic Aerodynamics and Heat Transfer of Re-Entry (Hardback)
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Specificaties
- Objectstaat
- Book Title
- Hypersonic Aerodynamics and Heat Transfer of Re-Entry Space Vehic
- Title
- Hypersonic Aerodynamics and Heat Transfer of Re-Entry Space Vehic
- EAN
- 9781567003093
- ISBN
- 9781567003093
- Release Date
- 31/07/2013
- Release Year
- 2013
- Country/Region of Manufacture
- US
- Item Length
- 185mm
- Genre
- Technology & Engineering
- Publication Year
- 2014
- Type
- Textbook
- Format
- Hardcover
- Subject Area
- Mechanical Engineering
- Language
- English
- Publication Name
- Hypersonic Aerodynamics and Heat Transfer of Re-Entry Space Vehicles and Planetary Probes
- Item Height
- 265 mm
- Publisher
- Begell House Publishers INC International Concepts concepts.,U.S.
- Item Width
- 185 mm
- Number of Pages
- 383 Pages
Over dit product
Product Information
Presents the results of theoretical and experimental studies of the problems of super/hypersonic flows around the models of real space vehicle configurations such as Buran -orbiter, winged cone (airplane-like body), Clipper space vehicle, and the Martian planetary probe. Theoretical analysis is based on solution 2/3D Navier- Stokes equations and their simplified asymptotic models with account for equilibrium and nonequilibrium chemical reactions taking place at the background of relaxation of excited internal energy modes of the particles in the shock layer and on the vehicle surface. Exact and simple relationships for the transport of species mass and heat are derived from rigorous kinetic theory for multicomponent mixtures of gases and plasma with different diffusion characteristics of the species (governing relations - thermodynamic parameter gradients expressed through the fluxes) as well as velocity slip, temperature and species concentration jumps boundary conditions for the surfaces of finite catalycity in multicomponent chemically and thermally nonequilibrium gas flow. Phenomenological and kinetic models are developed for heterogeneous catalytic reactions on the thermal protection materials of the space vehicles entering Earth and Mars atmospheres along gliding trajectories. The problem of multicomponent thermally and chemically nonequilibrium air flow in inductively coupled plasma torch and jet flow around the models installed in the facility work section in considered. The possibility to specify catalytic properties of real heat shield coatings are demonstrated using numerical and test values of heat fluxes or surface equilibrium radiation temperatures. The original iterative/marching method to solve viscous shock layer equations is presented. The method is based on the splitting of the marching component of the pressure gradient onto hyperbolic part and a part that minimizes the elliptic part to a maximum degree that are then subjected to the global iterations procedure. Using splitting of this kind allows the obtaining of the drug and heat transfer coefficients within single or couple global iterations. The knowledge area connected to development of large computer software for conjugate problem of ballistics, aerodynamics, vehicle heat transfer and thermal strength of constructions of variable mass and shape is developed for all stages of the modern rocket-space vehicle design.
Product Identifiers
Publisher
Begell House Publishers INC International Concepts concepts.,U.S.
ISBN-13
9781567003093
eBay Product ID (ePID)
209389998
Product Key Features
Subject Area
Mechanical Engineering
Publication Name
Hypersonic Aerodynamics and Heat Transfer of Re-Entry Space Vehicles and Planetary Probes
Format
Hardcover
Language
English
Publication Year
2014
Type
Textbook
Number of Pages
383 Pages
Dimensions
Item Height
265 mm
Item Width
185 mm
Additional Product Features
Country/Region of Manufacture
United States
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