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Wing Theory in Supersonic Flow

Wing Theory in Supersonic Flow
Author: Elie Carafoli
Publisher: Elsevier
Total Pages: 611
Release: 2013-10-22
Genre: Technology & Engineering
ISBN: 1483160270

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Division II: Aerodynamics, Volume 7: Wing Theory in Supersonic Flow examines the cases of isolated simple wings, wings with vertical plane tail, cruciform wings, and simple or cruciform wings fitted with a body. This book presents the method for the actual calculation of isolated wings or of more complex system. Organized into 12 chapters, this volume starts with an overview of the basic equations in the mechanics of inviscid fluids. This text then presents a unified theory that is established for angularly shaped wings in supersonic flow. Other chapters consider the method for calculating the characteristics of drag, lift, and moments for various shapes of the trailing edge line. This book discusses as well the wings of ordinary shapes, delta wings, yawed wings, polygonal wings, trapezoid wings, and arrow-head or swept-back wings. The final chapter deals with a delta wing with a central fusiform body. This book is a valuable resource for teachers, students, and specialists engaged in modern aerodynamics.


The Calculation of Downwash Behind Supersonic Wings with an Application to Triangular Plan Forms

The Calculation of Downwash Behind Supersonic Wings with an Application to Triangular Plan Forms
Author: Maxwell Alfred Heaslet
Publisher:
Total Pages: 52
Release: 1948
Genre: Aerodynamics, Supersonic
ISBN:

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A method is developed, consistent with the assumptions of small perturbation theory, which provides a means of determining for a known load distribution, the downwash behind a wing in supersonic flow. THe analysis is based upon the use of supersonic doublets which are distributed over the plan form and wake of the wing in a manner determined from the wing loading.


Two-dimensional Wing Theory in the Supersonic Range

Two-dimensional Wing Theory in the Supersonic Range
Author: H. Hönl
Publisher:
Total Pages: 764
Release: 1949
Genre: Aerodynamic load
ISBN:

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The plane problem of the vibrating airfoil in supersonic flow is dealt with and solved within the scope of a linearized theory by the method of the acceleration potential.


Wing Theory

Wing Theory
Author: A. Robinson
Publisher: Cambridge University Press
Total Pages: 583
Release: 2013-09-12
Genre: Technology & Engineering
ISBN: 1107622654

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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.


High Speed Wing Theory

High Speed Wing Theory
Author: Doris Cohen
Publisher: Princeton University Press
Total Pages: 251
Release: 2015-12-08
Genre: Technology & Engineering
ISBN: 1400874947

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Part of the Princeton Aeronautical Paperback series designed to bring to students and research engineers outstanding portions of the twelve-volume High Speed Aerodynamics and Jet Propulsion series. These books have been prepared by direct reproduction of the text from the original series and no attempt has been made to provide introductory material or to eliminate cross reference to other portions of the original volumes. Originally published in 1960. The Princeton Legacy Library uses the latest print-on-demand technology to again make available previously out-of-print books from the distinguished backlist of Princeton University Press. These editions preserve the original texts of these important books while presenting them in durable paperback and hardcover editions. The goal of the Princeton Legacy Library is to vastly increase access to the rich scholarly heritage found in the thousands of books published by Princeton University Press since its founding in 1905.


Wing Theory

Wing Theory
Author: Robert Thomas Jones
Publisher: Princeton University Press
Total Pages: 227
Release: 2014-07-14
Genre: Technology & Engineering
ISBN: 1400860776

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Originator of many of the theories used in modern wing design, Robert T. Jones surveys the aerodynamics of wings from the early theories of lift to modern theoretical developments. This work covers the behavior of wings at both low and high speeds, including the range from very low Reynolds numbers to the determination of minimum drag at supersonic speed. Emphasizing analytical techniques, Wing Theory provides invaluable physical principles and insights for advanced students, professors, and aeronautical engineers, as well as for scientists involved in computational approaches to the subject. This book is based on over forty years of theoretical and practical work performed by the author and other leading researchers in the field of aerodynamics. Originally published in 1990. The Princeton Legacy Library uses the latest print-on-demand technology to again make available previously out-of-print books from the distinguished backlist of Princeton University Press. These editions preserve the original texts of these important books while presenting them in durable paperback and hardcover editions. The goal of the Princeton Legacy Library is to vastly increase access to the rich scholarly heritage found in the thousands of books published by Princeton University Press since its founding in 1905.


Theoretical Relations Between the Stability Derivatives of a Wing in Direct and in Reverse Supersonic Flow

Theoretical Relations Between the Stability Derivatives of a Wing in Direct and in Reverse Supersonic Flow
Author: Sidney M. Harmon
Publisher:
Total Pages: 54
Release: 1949
Genre: Aerodynamics, Supersonic
ISBN:

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The investivation is made for thin flate-plate wings for steady vertical and longitudinal motions, setady rolling and pitching, and motions in which the wing is accelerating uniformly in the vertical direction.


Two-dimensional Wing Theory in the Supersonic Range

Two-dimensional Wing Theory in the Supersonic Range
Author: H. Honl
Publisher:
Total Pages: 25
Release: 1947
Genre: Aerodynamics, Supersonic
ISBN:

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The plane problem of the vibrating wing in supersonic flow is discussed and followed by the acceleration potential method, on the basis of a linearized theory.