Description and Evaluation of a Digital-Computer Program for Calculating the Viscous Drag of Bodies of Revolution PDF Download
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Author:
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Category :
Languages : en
Pages : 148
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Book Description
A digital-computer program has been written for calculating the viscous drag of streamlined bodies of revolution in constant-density axial flow. The integral approach adopted incorporates recently improved methods for predicting the transition point and for calculating the turbulent boundary layer. The inputs to the computer program are the body geometry, the associated inviscid pressure distribution, and the body-length Reynolds number. Agreement of calculated and measured drag coefficients is good, particularly in cases where the transition point is predicted accurately. (Author).
Author:
Publisher:
ISBN:
Category :
Languages : en
Pages : 148
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Book Description
A digital-computer program has been written for calculating the viscous drag of streamlined bodies of revolution in constant-density axial flow. The integral approach adopted incorporates recently improved methods for predicting the transition point and for calculating the turbulent boundary layer. The inputs to the computer program are the body geometry, the associated inviscid pressure distribution, and the body-length Reynolds number. Agreement of calculated and measured drag coefficients is good, particularly in cases where the transition point is predicted accurately. (Author).
Author: Keith P. Kerney
Publisher:
ISBN:
Category : Boundary layer
Languages : en
Pages : 145
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Book Description
A digital-computer program has been written for calculating the viscous drag of streamlined bodies of revolution in constant-density axial flow. The integral approach adopted incorporates recently improved methods for predicting the transition point and for calculating the turbulent boundary layer. The inputs to the computer program are the body geometry, the associated inviscid pressure distribution, and the body-length Reynolds number. Agreement of calculated and measured drag coefficients is good, particularly in cases where the transition point is predicted accurately. (Author).
Author:
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Category : Weights and measures
Languages : en
Pages : 520
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Book Description
Author:
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ISBN:
Category : Aeronautics
Languages : en
Pages : 1124
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Book Description
Author: United States. National Bureau of Standards
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ISBN:
Category : Hydraulic engineering
Languages : en
Pages : 384
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Book Description
Author: Pauline H. Gurewitz
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ISBN:
Category : Hydraulic engineering
Languages : en
Pages : 384
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Book Description
Author: Valentine Korah
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ISBN:
Category : Antitrust law
Languages : en
Pages : 2354
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Book Description
Author:
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ISBN:
Category : Computer programs
Languages : en
Pages : 36
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Book Description
Author:
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ISBN:
Category : Science
Languages : en
Pages : 256
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Book Description
Author: Charlie M. Jackson
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Category : Aerodynamics, Supersonic
Languages : en
Pages : 44
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Book Description
This report describes a theoretical method for estimating the aerodynamic loading on a wing-body configuration. In order to provide a basis for evaluation of the method, experimental measurements of surface pressures, forces, and moments were made on a series of basic wing-body configurations over a Mach number range from 2.5 to 4.5. Comparison of the theoretical estimates with these experimental data generally indicated good agreement for the entire range of configurations and test conditions.
