Theoretical Studies of Unsteady Transonic Flow. Part V. Solution for the Delta Wing and Wings of General Polygonal Planforms PDF Download
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Author: Marten T. Landahl
Publisher:
ISBN:
Category :
Languages : en
Pages : 22
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Book Description
Author: Marten T. Landahl
Publisher:
ISBN:
Category :
Languages : en
Pages : 22
Get Book Here
Book Description
Author: Marten T. Landahl
Publisher:
ISBN:
Category :
Languages : en
Pages :
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Book Description
Author: Marten T. Landahl
Publisher:
ISBN:
Category :
Languages : en
Pages : 22
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Book Description
Author: Mårten T. Landahl
Publisher: Courier Dover Publications
ISBN: 0486832775
Category : Science
Languages : en
Pages : 147
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Book Description
This classic monograph on unsteady transonic flow — the flow of air encountered at speeds at or near the speed of sound — is of continuing interest to students and professionals in aerodynamics, fluid dynamics, and other areas of applied mathematics. After a brief Introduction, Swedish physicist Mårten T. Landahl presents a chapter in which the two-dimensional solution is derived, succeeded by a discussion of its relation to the subsonic and supersonic solutions. Three chapters on low aspect ratio configurations follow, covering triangular wings and similar planforms with curved leading edges, rectangular wings, and cropped delta wings, and low aspect ratio wing-body combinations. The treatment concludes with a consideration of the experimental determination of air forces on oscillating wings at transonic speeds.
Author: Mårten T. Landahl
Publisher:
ISBN:
Category :
Languages : en
Pages : 22
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Book Description
Author: Marten T. Landahl
Publisher: Courier Dover Publications
ISBN: 0486839907
Category : Science
Languages : en
Pages : 147
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Book Description
This classic monograph on unsteady transonic flow — the flow of air encountered at speeds at or near the speed of sound — is of continuing interest to students and professionals in aerodynamics, fluid dynamics, and other areas of applied mathematics. After a brief Introduction, Swedish physicist Mårten T. Landahl presents a chapter in which the two-dimensional solution is derived, succeeded by a discussion of its relation to the subsonic and supersonic solutions. Three chapters on low aspect ratio configurations follow, covering triangular wings and similar planforms with curved leading edges, rectangular wings, and cropped delta wings, and low aspect ratio wing-body combinations. The treatment concludes with a consideration of the experimental determination of air forces on oscillating wings at transonic speeds.
Author:
Publisher:
ISBN:
Category : Mechanics, Applied
Languages : en
Pages : 1006
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Book Description
Author: Flygtekniska försöksanstalten (Sweden)
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 460
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Book Description
Author: North Atlantic Treaty Organization. Advisory Group for Aerospace Research and Development. Structures and Materials Panel
Publisher:
ISBN:
Category : Aeroelasticity
Languages : en
Pages : 686
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Book Description
Author: North Atlantic Treaty Organization. Advisory Group for Aeronautical Research and Development. Structures and Materials Panel
Publisher:
ISBN:
Category : Aeroelasticity
Languages : en
Pages : 716
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