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Author: Nikolaĭ Fedorovich Krasnov
Publisher: Elsevier Publishing Company
ISBN:
Category : Science
Languages : en
Pages : 930
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Book Description
A comprehensive technical treatise is provided on the aerodynamics of bodies of revolution from transonic to hypersonic speeds, covering all aspects of the subject, including transonic flow, linearized supersonic flow, Newtonian flow, rarefield gas and free-molecule flow, skin friction, heat transfer, and mass transfer. This English translation of a unique Russian textbook is provided with some corrections, references for all sources the editor could identify, redrawn figures, and an editor's introduction to each chapter summarizing and referencing pertinent material that has appeared since 1964, when the second edition was published. Krasnov's general approach assumes knowledge of the basic gas dynamic equations and applies them to solve aerodynamic problems. All important methods and techniques in modern aerodynamic theory are developed, with the aim of presenting practical methods for solving engineering problems. Results are usually given in the form of working equations, graphs, tables, or detailed sequential calculation methods. (Author).
Author: Nikolaĭ Fedorovich Krasnov
Publisher: Elsevier Publishing Company
ISBN:
Category : Science
Languages : en
Pages : 930
Get Book Here
Book Description
A comprehensive technical treatise is provided on the aerodynamics of bodies of revolution from transonic to hypersonic speeds, covering all aspects of the subject, including transonic flow, linearized supersonic flow, Newtonian flow, rarefield gas and free-molecule flow, skin friction, heat transfer, and mass transfer. This English translation of a unique Russian textbook is provided with some corrections, references for all sources the editor could identify, redrawn figures, and an editor's introduction to each chapter summarizing and referencing pertinent material that has appeared since 1964, when the second edition was published. Krasnov's general approach assumes knowledge of the basic gas dynamic equations and applies them to solve aerodynamic problems. All important methods and techniques in modern aerodynamic theory are developed, with the aim of presenting practical methods for solving engineering problems. Results are usually given in the form of working equations, graphs, tables, or detailed sequential calculation methods. (Author).
Author: Nikolai F. Krasnov
Publisher:
ISBN:
Category :
Languages : en
Pages : 169
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Book Description
Aerodynamic forces and moments; the basic features of very high velocity gas flow; the basic concepts and equations for determining the flow parameters; Basic relations for determining gas parameters behind a shock wave; Results from boundary-layer and heattransfer theory.
Author: Holt Ashley
Publisher: Courier Corporation
ISBN: 0486648990
Category : Technology & Engineering
Languages : en
Pages : 306
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Book Description
This excellent, innovative reference offers a wealth of useful information and a solid background in the fundamentals of aerodynamics. Fluid mechanics, constant density inviscid flow, singular perturbation problems, viscosity, thin-wing and slender body theories, drag minimalization, and other essentials are addressed in a lively, literate manner and accompanied by diagrams.
![Aerodynamics of Bodies of Revolution [by] N.F. Krasnov. Edited and Annotated by Deane N. Morris. Translated from the 2d Russian Ed. by Joy E. Gazley PDF](https://books.google.com/books/content/images/frontcover/7pchcgAACAAJ?fife=w80-h100)
Author: Nikolaĭ Fedorovich Krasnov
Publisher:
ISBN:
Category : Aerodynamics, Supersonic
Languages : en
Pages : 895
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Book Description
Author: D. Adamson
Publisher:
ISBN:
Category : Aerodynamics, Supersonic
Languages : en
Pages : 366
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Book Description
Author: Reuben Bond
Publisher:
ISBN:
Category : Aerodynamics, Supersonic
Languages : en
Pages : 36
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Book Description
Linearized slender-body theory is applied to the computation of aerodynamic forces on an oscillating, or deforming, body in supersonic flow. The undeformed body is a body of revolution and the deformed body is represented by movement of a line through the centers of the cross sections which are assumed to remain circular. The time dependence is based on sinusoidal motion. For a body of vanishing thickness the slender-body theory yields the apparent mass approximation as it is obtained for incompressible crossflow around a cylinder. Both linearized slender-body theory and the apparent mass approximation are used to calculate the pitching-moment coefficients on a rigid slender body with a parabolic arc nose cone, and these coefficients are compared with some experimental results. (Author).
Author: Waldo I. Oehman
Publisher:
ISBN:
Category : Aerodynamics, Hypersonic
Languages : en
Pages : 60
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Book Description
Minimum drag bodies in hypersonic flow using calculus of variations.
Author: Nikolai Fedorovich Krasnov
Publisher:
ISBN:
Category : Aerodynamics, Supersonic
Languages : en
Pages : 895
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Book Description
Author: JOHNS HOPKINS UNIV SILVER SPRING MD APPLIED PHYSICS LAB.
Publisher:
ISBN:
Category :
Languages : en
Pages : 365
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Book Description
This section of the Handbook presents data on the aerodynamic characteristics of bodies of revolution for an angle-of-attack range of zero to almost ninety degrees throughout the supersonic and hypersonic flight regimes. Basic theories governing the pressure distributions on bodies of revolution and in their surrounding flow fields are discussed and evaluated. To provide a basis for the selection of theoretical methods to be used in specific calculation the reliability and accuracy of these theories are compared at different Mach and Reynolds numbers. Actual step-by-step development is omitted except where it is essential to an understanding of resultant expressions. In all cases, however, sources containing full derivations are referenced. To permit comparison or extension of the theoretical methods, experimentally-derived data in many instances are also presented. For those cases in which there is discrepancy between theory and experiment, empirical formulae are given together with the limiting values of the parameters within which the particular formula is valid. Techniques for incorporating the effects of skin friction and heat transfer (treated fully in Sections 13 and 14 of the Handbook) are also given.
Author: Edward E. Mayo
Publisher:
ISBN:
Category : Newtonian cosmology
Languages : en
Pages : 36
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Book Description
