Analysis of the Linearized Supersonic Flow about Pointed Bodies of Revolution by the Method of Characteristics PDF Download
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Author: Alan D. Sherer
Publisher:
ISBN:
Category : Aerodynamics, Supersonic
Languages : en
Pages : 52
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Book Description
Author: Alan D. Sherer
Publisher:
ISBN:
Category : Aerodynamics, Supersonic
Languages : en
Pages : 52
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Book Description
Author: Wallace Dean Hayes
Publisher:
ISBN:
Category : Aerodynamics, Supersonic
Languages : en
Pages : 348
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Book Description
Author: Zdeněk Kopal
Publisher:
ISBN:
Category : Aerodynamics, Supersonic
Languages : en
Pages : 20
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Book Description
Author: C. N. Ward
Publisher:
ISBN:
Category :
Languages : en
Pages :
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Book Description
Author: F. Edward Ehlers
Publisher:
ISBN:
Category : Aerodynamics, Supersonic
Languages : en
Pages : 260
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Book Description
Author: G. N. Ward
Publisher: Cambridge University Press
ISBN: 1316601897
Category : Mathematics
Languages : en
Pages : 261
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Book Description
Originally published in 1955, this book is devoted exclusively to the problems involved in solving the non-linear equations of motion for compressible fluids.
Author: G. N. Ward
Publisher:
ISBN:
Category :
Languages : en
Pages : 14
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Book Description
Author: Sydney Goldstein
Publisher:
ISBN:
Category : Aerodynamics, Supersonic
Languages : en
Pages : 56
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Book Description
Author: George K. Morikawa
Publisher:
ISBN:
Category : Electronic dissertations
Languages : en
Pages : 138
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Book Description
Author: Vincent Robert Mascitti
Publisher:
ISBN:
Category : Aerodynamics, Supersonic
Languages : en
Pages : 52
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Book Description
Supersonic linearized conical-flow theory is used to determine the flow over slender pointed cones having horizontal and vertical planes of symmetry. The geometry of the cone cross sections and surface velocities are expanded in Fourier series. The symmetry condition permits the uncoupling of lifting and nonlifting solutions. The present method reduces to Ward's theory for flow over a cone of elliptic cross section. Results are also presented for other shapes. Results by this method diverge for cross-sectional shapes where the maximum thickness is large compared with the minimum thickness. However, even for these slender-body shapes, lower order solutions are good approximations to the complete solution.
