Tables for Supersonic Flow Around Right Circular Cones at Zero Angle of Attack PDF Download
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Author: Joseph L. Sims
Publisher:
ISBN:
Category : Aerodynamics, Supersonic
Languages : en
Pages : 428
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Book Description
Author: Joseph L. Sims
Publisher:
ISBN:
Category : Aerodynamics, Supersonic
Languages : en
Pages : 428
Get Book Here
Book Description
Author: Joseph L. Sims
Publisher:
ISBN:
Category : Aerodynamics, Supersonic
Languages : en
Pages : 440
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Book Description
Author: Joseph L. Sims
Publisher:
ISBN:
Category : Aerodynamics, Supersonic
Languages : en
Pages : 444
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Book Description
Author: Joseph L. Sims
Publisher:
ISBN:
Category : Aerodynamics, Supersonic
Languages : en
Pages : 882
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Book Description
Author: Joseph L. Sims
Publisher:
ISBN:
Category : Aerodynamics, Supersonic
Languages : en
Pages : 36
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Book Description
The results of the calculation of supersonic flow of helium about right circular cones at zero angle of attack are presented in tabular form. The calculations were performed using the Taylor-Maccoll theory. Numerical integrations were performed using a Runge-Kutta method for second-order differential equations. Results were obtained for cone angles from 2.5 to 30 degrees in regular increments of 2.5 degrees. In all calculations the desired free-stream Mach number was obtained to five or more significant figures.
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Author:
Publisher:
ISBN:
Category : Aerodynamics, Supersonic
Languages : en
Pages : 421
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Book Description
Author: Joseph L. Sims
Publisher:
ISBN:
Category :
Languages : en
Pages : 24
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Book Description
Author: Joseph L. Sims
Publisher:
ISBN:
Category :
Languages : en
Pages : 421
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Book Description
Author: Joseph L. Sims
Publisher:
ISBN:
Category : Aerodymanics, Supersonic
Languages : en
Pages : 432
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Book Description
Author: J. L. Sims
Publisher:
ISBN:
Category :
Languages : en
Pages : 421
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Book Description
