Experimental Study of the Supersonic Flow Around V-Shaped Wings PDF Download
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Author: A. L. Gonor
Publisher:
ISBN:
Category :
Languages : en
Pages : 30
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Author: A. L. Gonor
Publisher:
ISBN:
Category :
Languages : en
Pages : 30
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Author:
Publisher:
ISBN:
Category :
Languages : en
Pages : 74
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Author: Chuan Fang Chen
Publisher:
ISBN:
Category :
Languages : en
Pages : 142
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Author:
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ISBN:
Category : Science
Languages : en
Pages : 1048
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Author: Hakuro Oguchi
Publisher:
ISBN:
Category :
Languages : en
Pages :
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Author: Dean R. Chapman
Publisher:
ISBN:
Category : Aerodynamics, Supersonic
Languages : en
Pages : 852
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Book Description
The pressres acting on the base of blunt-trailing-edge airfoils have been measured at Mach numbers of 1.25, 1.5, 2.0, and 3.1 and at Reynolds numbers from 0.2 to 3.8 million. Data are presented for 29 profiles both with laminar and with turbulent boundary layers approaching the trailing edges of the wings. The base pressure is found to be a function primarily of Mach number and the ratio of the boundary layer thickeness at the trailing edge to the trailing-edge thickness.
Author: Elie Carafoli
Publisher: Elsevier
ISBN: 1483160270
Category : Technology & Engineering
Languages : en
Pages : 611
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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.
Author:
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ISBN:
Category : Mechanics, Applied
Languages : en
Pages : 592
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Author:
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Category : Aeronautics
Languages : en
Pages : 702
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Author: I.C. Richards
Publisher:
ISBN:
Category :
Languages : en
Pages : 6
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