A Thin Wing In A Compressible Flow
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A Thin Wing In A Compressible Flow
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Author :
language : en
Publisher:
Release Date : 1982
A Thin Wing In A Compressible Flow written by and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1982 with categories.
A Thin Wing In A Compressible Flow
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Author : E. A. Krasilʹshchikova
language : en
Publisher: Springer
Release Date : 1982
A Thin Wing In A Compressible Flow written by E. A. Krasilʹshchikova and has been published by Springer this book supported file pdf, txt, epub, kindle and other format this book has been release on 1982 with Science categories.
A Thin Wing In A Compressible Flow
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Author : Elena A. Krasil'ščikova
language : en
Publisher:
Release Date : 1983
A Thin Wing In A Compressible Flow written by Elena A. Krasil'ščikova and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1983 with categories.
Finite Span Wings In Compressible Flow
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Author : E. A. Krasilʹshchikova
language : en
Publisher:
Release Date : 1956
Finite Span Wings In Compressible Flow written by E. A. Krasilʹshchikova and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1956 with Aerodynamics categories.
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.
Subsonic Edges In Thin Wing And Slender Body Theory
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Author : Milton D. Van Dyke
language : en
Publisher:
Release Date : 1954
Subsonic Edges In Thin Wing And Slender Body Theory written by Milton D. Van Dyke and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1954 with Aerofoils categories.
A simple technique is presented for correcting the results of thin-wing theory near round or sharp edges at which the normal component of free-stream velocity is subsonic. The flow in planes normal to such edges is actually brought to rest, but thin-wing theory instead predicts infinite velocities. Furthermore, corresponding to the circulatory flow around leading edges, thin-wing theory predicts additional singularities that do not actually exist for round edges and exceed their true strength for sharp edges. All these singularities grow worse if one formally attempts to improve the solution by iteration. To correct these defects, the formal thin-wing solution is here rendered uniformly valid by comparing with exact solutions for simple profiles having the same nose shape. In this way Lighthill's rule for correcting the surface speed on round-nosed airfoils in incompressible flow is extended to higher approximations, to compressible flow, to three-dimensional wings, and to sharp edges. Corresponding results for slender bodies of revolution are considered briefly; in particular, the rules for round-nosed airfoils in incompressble flow are shown to apply also to round-nosed bodies of revolution.
A Method For Calculating Aerodynamic Loadings On Thin Wings At A Mach Number Of 1
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Author : John L. Crigler
language : en
Publisher:
Release Date : 1959
A Method For Calculating Aerodynamic Loadings On Thin Wings At A Mach Number Of 1 written by John L. Crigler and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1959 with Aerodynamic load categories.
A Cruciform Wing Of Finite Span In A Compressible Flow
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Author : B. I. Fridlender
language : en
Publisher:
Release Date : 1964
A Cruciform Wing Of Finite Span In A Compressible Flow written by B. I. Fridlender and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1964 with categories.
The aerodynamic characteristics of a thin, cruciform wing consisting of four consoles of arbitrary geometric form are mathematical analyzed.
Theoretical Computational Dynamics
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Author : Pai
language : en
Publisher: CRC Press
Release Date : 1997-03-01
Theoretical Computational Dynamics written by Pai and has been published by CRC Press this book supported file pdf, txt, epub, kindle and other format this book has been release on 1997-03-01 with Mathematics categories.
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
Linearized Theory Of Steady High Speed Flow
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Author :
language : en
Publisher: CUP Archive
Release Date :
Linearized Theory Of Steady High Speed Flow written by and has been published by CUP Archive this book supported file pdf, txt, epub, kindle and other format this book has been release on with categories.
A Method For Calculating Aerodynamic Loadings On Thin Wings At A Mach Number Of 1
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Author : John L. Crigler
language : en
Publisher:
Release Date : 1959
A Method For Calculating Aerodynamic Loadings On Thin Wings At A Mach Number Of 1 written by John L. Crigler and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1959 with Aerodynamic load categories.