Author: Publisher:
ISBN:
Category :
Languages : en
Pages :
Book Description
A Thin Wing in a Compressible Flow
Author: A Thin Wing in a Compressible Flow
Author: E. A. KrasilʹshchikovaPublisher: Springer
ISBN:
Category : Science
Languages : en
Pages : 256
Book Description
A thin wing in a compressible flow
Author: Elena A. Krasil'ščikovaFinite Span Wings in Compressible Flow
Author: E. A. KrasilʹshchikovaPublisher:
ISBN:
Category : Aerodynamics
Languages : en
Pages : 138
Book Description
Abstract: Equations are developed using the source distribution method for the velocity potential function and pressure on thin wings in steady and unsteady motion. Closed form solutions are given for harmonically oscillating wings of general plan form including the effect of the wing wake. Some useful examples are presented in an appendix for arrow, semielliptical, and hexagonal plan form wings. The paper is essentially a summary of previous work by the author.
Waves and Compressible Flow
Author: Hilary OckendonPublisher: Springer Science & Business Media
ISBN: 0387218025
Category : Mathematics
Languages : en
Pages : 193
Book Description
This book covers compressible flow however the authors also show how wave phenomena in electromagnetism and solid mechanics can be treated using similar mathematical methods. It caters to the needs of the modern student by providing the tools necessary for a mathematical analysis of most kinds of waves liable to be encountered in modern science and technology. At the same time emphasis is laid on the physical background and modeling that requires these tools.
Basic Aerodynamics
Author: Gary A. FlandroPublisher: Cambridge University Press
ISBN: 1139498614
Category : Technology & Engineering
Languages : en
Pages : 433
Book Description
In the rapidly advancing field of flight aerodynamics, it is especially important for students to master the fundamentals. This text, written by renowned experts, clearly presents the basic concepts of underlying aerodynamic prediction methodology. These concepts are closely linked to physical principles so that they are more readily retained and their limits of applicability are fully appreciated. Ultimately, this will provide students with the necessary tools to confidently approach and solve practical flight vehicle design problems of current and future interest. This book is designed for use in courses on aerodynamics at an advanced undergraduate or graduate level. A comprehensive set of exercise problems is included at the end of each chapter.
Theoretical Computational Dynamics
Author: PaiPublisher: CRC Press
ISBN: 9780442303105
Category : Mathematics
Languages : en
Pages : 724
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
A Method for Calculating Aerodynamic Loadings on Thin Wings at a Mach Number of 1
Author: John L. CriglerPublisher:
ISBN:
Category : Aerodynamic load
Languages : en
Pages : 34
Book Description
Wing Theory
Author: A. RobinsonPublisher: Cambridge University Press
ISBN: 1107622654
Category : Technology & Engineering
Languages : en
Pages : 583
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.
A Cruciform Wing of Finite Span in a Compressible Flow
Author: B. I. FridlenderPublisher:
ISBN:
Category :
Languages : en
Pages : 9
Book Description
The aerodynamic characteristics of a thin, cruciform wing consisting of four consoles of arbitrary geometric form are mathematical analyzed.