Linearized Theory of Steady High-Speed Flow PDF Download
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Author: G. N. Ward
Publisher: Cambridge University Press
ISBN: 1316601897
Category : Mathematics
Languages : en
Pages : 261
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Book Description
Originally published in 1955, this book is devoted exclusively to the problems involved in solving the non-linear equations of motion for compressible fluids.
Author: G. N. Ward
Publisher: Cambridge University Press
ISBN: 1316601897
Category : Mathematics
Languages : en
Pages : 261
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Book Description
Originally published in 1955, this book is devoted exclusively to the problems involved in solving the non-linear equations of motion for compressible fluids.
Author: Sydney Goldstein
Publisher:
ISBN:
Category : Aerodynamics, Supersonic
Languages : en
Pages : 56
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Book Description
Author: F. Edward Ehlers
Publisher:
ISBN:
Category : Aerodynamics, Supersonic
Languages : en
Pages : 260
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Book Description
Author: Shih-I Pai
Publisher: CRC Press
ISBN: 1000109860
Category : Mathematics
Languages : en
Pages : 700
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Book Description
This book gives an introduction to the theoretical and computational fluid dynamics of a compressible fluid. It focuses on the basic assumptions and the formulation of the theory of compressible flow as well as on the methods of solving problems.
Author: Pai
Publisher: CRC Press
ISBN: 9780442303105
Category : Mathematics
Languages : en
Pages : 724
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Book Description
Emphasis of this text is on the basic assumptions and the formulation of the theory of compressible flow as well as on the methods of solving problems. Published by Science Press, Beijing, distributed by VNR in the US. Annotation copyrighted by Book News, Inc., Portland, OR
Author: A. Robinson
Publisher: Cambridge University Press
ISBN: 1107622654
Category : Technology & Engineering
Languages : en
Pages : 583
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Book Description
First published in 1956 as part of the Cambridge Aeronautical Series, this book addresses the vital science of wing theory. Robinson and Laurmann record the historic developments in wing theory, including the work of Joukowski and Bernoulli, and discuss developments in supersonic flow and unsteady aerofoil theory. This book will be of value to anyone with an interest in the history of the science of flight.
Author: Rashad M. El Badrawy
Publisher:
ISBN:
Category : Aerodynamic load
Languages : en
Pages : 142
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Book Description
Abstract: A brief review of exact two-dimensional supersonic flow theory and Ackeret's linearized theory are first presented. The lift and drag coefficients of a cascade of flat plates are calculated exactly and compared to those obtained using the linearized theory. The forces on the cascade are determined for unsteady inlet flow. The flat plate cascade theory is extended to compute the efficiency of a supersonic propeller with friction and finite blade thickness.
Author:
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 588
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Book Description
Author: A. J. Eggers
Publisher:
ISBN:
Category : Aerodynamic heating
Languages : en
Pages : 324
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Book Description
Author: C.A. Truesdell
Publisher: Springer Science & Business Media
ISBN: 3642459447
Category : Science
Languages : en
Pages : 822
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Book Description
Sect 2. 317 tinuity surfaces 1. This suggests that a wake pressure Pw be associated with each flow past a bluff body, and that a wake parameter (2. 4) which plays the same role as the cavitation parameter (2. 1), be defined for the flow. This idea has been made the basis of a modified wake theory (ef. Sect. 11) which proves to be in good qu- titative agreement with pressure and drag measurements. It should be emphasized, however, that un h like the cavitation number, the wake parameter is a quantity which is not known a priori, and must be empirically determined in each case. (3) Jet flows. The problem of jet efflux from an orifice is one of the oldest in hydrodynamics and the first to be treated by Fig. 3a. the HELMHOLTZ free streamline theory. Of particular importance for engineering applications is the discharge coefficient Cd' which is defined in terms of the discharge Q per unit time, the pressure P, and the cross-sectional area A of the orifice, by the formula, (2. 5) where e is the fluid density. Two methods of measuring Cd have been most fre quently adopted. In the first the liquid issues from an orifice in a large vessel under the influence of gravity _,-____________ . , (Fig. 3 a), while in the second it 1 L is forced out of a nozzle or pipe under high pressure (Fig. 3 b).
