Study of the Two-dimensional Flow Through a Converging-diverging Nozzle PDF Download
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Author: Arthur Kantrowitz
Publisher:
ISBN:
Category :
Languages : en
Pages : 6
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Author: Arthur Kantrowitz
Publisher:
ISBN:
Category :
Languages : en
Pages : 6
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Author: Mary L. Mason
Publisher:
ISBN:
Category : Aerodynamics
Languages : en
Pages : 76
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Author: James Joe Der
Publisher:
ISBN:
Category : Aerodynamics, Supersonic
Languages : en
Pages : 64
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Book Description
Chemical and vibrational nonequilibrium phenomena in steady inviscid flow fields are studied by the analysis of flow past curved boundaries. Possible alternative choices of the state variables to be used are considered. General features of the nonequilibrium flow are studied by examination of the mathematical properties of the nonlinear flow equations. An axisymmetric nonequilibrium flow of air through a supersonic nozzle is analyzed by means of numerical computations. The coupling effects between nonuniformity (across a nozzle section) and nonequilibrium, not taken into account in the quasi-one-dimensional flow approximation, are revealed by the present analysis.
Author: Mary L. Mason
Publisher:
ISBN:
Category : Aerodynamics
Languages : en
Pages : 76
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Author: Hai-Tien Loh
Publisher:
ISBN:
Category :
Languages : en
Pages :
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Author: United States. National Advisory Committee for Aeronautics
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 616
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Author: K. Oswatitsch
Publisher: BiblioGov
ISBN: 9781289104917
Category :
Languages : en
Pages : 46
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Book Description
The present report describes a new method for the prediction of the flow pattern of a gas in the two-dimensional and axially symmetrical case. It is assumed that the expansion of the gas is adiabatic and the flow stationary. The several assumptions necessary of the nozzle shape effect, in general, no essential limitation on the conventional nozzles. The method is applicable throughout the entire speed range; the velocity of sound itself plays no singular part. The principal weight is placed on the treatment of the flow near the throat of a converging-diverging nozzle. For slender nozzles formulas are derived for the calculation of the velocity components as function of the location.
Author: Robert J. Simoneau
Publisher:
ISBN:
Category : Low temperature engineering
Languages : en
Pages : 88
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Author:
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 400
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Author: Thomas Harry Lindsey
Publisher:
ISBN:
Category :
Languages : en
Pages : 128
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