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Finite Span Wings In Compressible Flow
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Book Synopsis Finite Span Wings in Compressible Flow by : E. A. Krasilʹshchikova
Download or read book Finite Span Wings in Compressible Flow written by E. A. Krasilʹshchikova and published by . This book was released on 1956 with total page 138 pages. Available in PDF, EPUB and Kindle. Book excerpt: 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.
Book Synopsis Extension of the Theory of Oscillating Airfoils of Finite Span in Subsonic Compressible Flow by : Eric Reissner
Download or read book Extension of the Theory of Oscillating Airfoils of Finite Span in Subsonic Compressible Flow written by Eric Reissner and published by . This book was released on 1951 with total page 22 pages. Available in PDF, EPUB and Kindle. Book excerpt: As part of an investigation of flows around and forces on an oscillating finite wing in subsonic compressible flow, the exact double integrals occurring in the theoretical formulation of the three-dimensional nonstationary aerodynamic forces have previously been reduced to single integrals over the range of either one of the two independent variables. The present report describes a method for solving the resultant three-dimensional problem based on a generalization of approximate methods for solving two-dimensional problems. It is shown that the calculation of three-dimensional corrections to the two-dimensional integral equation for spanwise variation of circulation, provided tabulated values for the kernal of the integral equation are available.
Book Synopsis A Cruciform Wing of Finite Span in a Compressible Flow by : B. I. Fridlender
Download or read book A Cruciform Wing of Finite Span in a Compressible Flow written by B. I. Fridlender and published by . This book was released on 1964 with total page 9 pages. Available in PDF, EPUB and Kindle. Book excerpt: The aerodynamic characteristics of a thin, cruciform wing consisting of four consoles of arbitrary geometric form are mathematical analyzed.
Book Synopsis On the Theory of Oscillating Airfoils of Finite Span in Subsonic Compressible Flow by : Eric Reissner
Download or read book On the Theory of Oscillating Airfoils of Finite Span in Subsonic Compressible Flow written by Eric Reissner and published by . This book was released on 1949 with total page 44 pages. Available in PDF, EPUB and Kindle. Book excerpt: The present report is concerned with the problem of the oscillating airfoil of finite span, within the frame of the linearized lifting surface theory. The aim of this study is the development of a theory which incorporates simultaneously the effects of three-dimensionality of the flow and of compressibility of the fluid. As an exact solution of this problem, even within the limitations of the linearized theory, presents very great difficulties, it is worth while to work toward an approximate theory which is valid provided the aspect ratio of the lifting surface is not too small.
Book Synopsis Finite Span Wings in Compressiible Flow by : E. A. Krasilʹshchikova
Download or read book Finite Span Wings in Compressiible Flow written by E. A. Krasilʹshchikova and published by . This book was released on 1954 with total page 130 pages. Available in PDF, EPUB and Kindle. Book excerpt: This work is devoted to the study of the perturbations of an airstream by the motion of a slender wing at supersonic speeds.
Book Synopsis Use of Experimental Steady-flow Aerodynamic Parameters in the Calculation of Flutter Characteristics for Finite-span Swept Or Unswept Wings at Subsonic, Transonic, and Supersonic Speed by : Edward Carson Yates
Download or read book Use of Experimental Steady-flow Aerodynamic Parameters in the Calculation of Flutter Characteristics for Finite-span Swept Or Unswept Wings at Subsonic, Transonic, and Supersonic Speed written by Edward Carson Yates and published by . This book was released on 1960 with total page 56 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis A Thin Wing in a Compressible Flow by : E. A. Krasilʹshchikova
Download or read book A Thin Wing in a Compressible Flow written by E. A. Krasilʹshchikova and published by Springer. This book was released on 1982 with total page 256 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Determination of the Elastic Constants of Airplane Tires by :
Download or read book Determination of the Elastic Constants of Airplane Tires written by and published by . This book was released on 1954 with total page 680 pages. Available in PDF, EPUB and Kindle. Book excerpt: For determination of the elastic constants of airplane tires which are required for the numerical calculations of the shimmy properties of nose and tail wheels, deformation measurements were carried out on four different tires. For this purpose, the tires were loaded in each case with a normal load and then with a lateral force, a tangential force, and a moment. Moreover, the weight and the mass moment of inertia about a vertical axis were determined for the various tires.
Book Synopsis Subsonic Aerodynamics by : Ion Paraschivoiu
Download or read book Subsonic Aerodynamics written by Ion Paraschivoiu and published by Presses inter Polytechnique. This book was released on 2003 with total page 568 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Unsteady Motion of a Wing of Finite Span in a Compressible Medium by : E. A. KRASILSHCHIKOVA
Download or read book Unsteady Motion of a Wing of Finite Span in a Compressible Medium written by E. A. KRASILSHCHIKOVA and published by . This book was released on 1961 with total page 1 pages. Available in PDF, EPUB and Kindle. Book excerpt: The linearized boundary value problem for the velocity potential for steady or unsteady finite wings in a compressible medium is formulated. The general equation for the velocity potential is given in the form of integrals of source distributions. The local source strength, determined in previous investigations (for example, in NACA TM-1383 AD 107 582), is proportional to local downwash, but the region that must be covered by sources, as well as the domain of integration, must extend over all points of the xyplane from which disturbances can affect the potential. (Author).
Book Synopsis An Introduction to the Theory of Aeroelasticity by : Y C Fung
Download or read book An Introduction to the Theory of Aeroelasticity written by Y C Fung and published by Courier Dover Publications. This book was released on 2008-10-17 with total page 516 pages. Available in PDF, EPUB and Kindle. Book excerpt: Geared toward advanced undergraduates and graduate students, this outstanding text surveys aeroelastic problems, their historical background, basic physical concepts, and the principles of analysis.
Book Synopsis Technical Memorandums by : United States. National Advisory Committee for Aeronautics
Download or read book Technical Memorandums written by United States. National Advisory Committee for Aeronautics and published by . This book was released on 1955 with total page 510 pages. Available in PDF, EPUB and Kindle. Book excerpt: Chiefly translations from foreign aeronautical journals.
Book Synopsis Principles of Aeroelasticity by : Raymond L. Bisplinghoff
Download or read book Principles of Aeroelasticity written by Raymond L. Bisplinghoff and published by Courier Corporation. This book was released on 2013-10-17 with total page 545 pages. Available in PDF, EPUB and Kindle. Book excerpt: Geared toward professional engineers, this volume will be helpful for students, too. Topics include methods of constructing static and dynamic equations, heated elastic solids, forms of aerodynamic operators, structural operators, and more. 1962 edition.
Book Synopsis Report by : United States. National Advisory Committee for Aeronautics
Download or read book Report written by United States. National Advisory Committee for Aeronautics and published by . This book was released on 1957 with total page 40 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Download or read book Applied Mechanics Reviews written by and published by . This book was released on 1970 with total page 796 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Aeroelasticity by : Raymond L. Bisplinghoff
Download or read book Aeroelasticity written by Raymond L. Bisplinghoff and published by Courier Corporation. This book was released on 2013-06-18 with total page 882 pages. Available in PDF, EPUB and Kindle. Book excerpt: Designed as both a textbook for advanced engineering students and a reference book for practicing engineers, this highly regarded work deals not only with the practical aspects of aeroelasticity, but the aerodynamic and structural tools upon which these rest. Accordingly, the book divides roughly into two halves: the first deals with the tools and the second with applications of the tools to aeroelastic phenomena. Topics include deformation of airplane structures under static and dynamic loads, approximate methods of computing natural mode shapes and frequencies, two-and three-dimensional incompressible flow, compressible flow, wings and bodies in three-dimensional unsteady flow, static aeroelastic phenomena, flutter, dynamic response phenomena, aeroelastic model theory, model design and construction, testing techniques and more. Chapters have been designed to progress from easy to difficult so that instructors using this book as an elementary text in aeroelasticity will find their purposes served by simply using the first parts of selected chapters. Helpful appendixes deal with such mathematical tools as matrices and linear systems (prerequisites include the usual engineering mathematics courses and advanced calculus), while many numerical examples are included throughout the text. Engineering students as well as practicing engineers will find this work an unmatched treatment of the topic and an indispensable reference for their libraries.
Book Synopsis Annual Report - National Advisory Committee for Aeronautics by : United States. National Advisory Committee for Aeronautics
Download or read book Annual Report - National Advisory Committee for Aeronautics written by United States. National Advisory Committee for Aeronautics and published by . This book was released on 1957 with total page pages. Available in PDF, EPUB and Kindle. Book excerpt: Includes the Committee's Technical reports no. 1-1058, reprinted in v. 1-37.
