Author: V. I. Timoshenko
Publisher:
ISBN:
Category :
Languages : en
Pages : 5

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Book Description

Author:
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 1146

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Book Description

Author:
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 548

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Book Description

Author:
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 580

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Book Description
A selection of annotated references to unclassified reports and journal articles that were introduced into the NASA scientific and technical information system and announced in Scientific and technical aerospace reports (STAR) and International aerospace abstracts (IAA)

Author:
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 992

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Author:
Publisher:
ISBN:
Category : Science
Languages : en
Pages : 1186

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Author:
Publisher:
ISBN:
Category : Mechanics, Applied
Languages : en
Pages : 736

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Author:
Publisher:
ISBN:
Category : Military research
Languages : en
Pages : 592

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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.

Author: Adriana Nastase
Publisher: Elsevier
ISBN: 008055699X
Category : Technology & Engineering
Languages : en
Pages : 425

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Book Description
Computation of Supersonic Flow over Flying Configurations is a high-level aerospace reference book that will be useful for undergraduate and graduate students of engineering, applied mathematics and physics. The author provides solutions for three-dimensional compressible Navier-Stokes layer subsonic and supersonic flows. - Computational work and experimental results show the real-world application of computational results - Easy computation and visualization of inviscid and viscous aerodynamic characteristics of flying configurations - Includes a fully optimized and integrated design for a proposed supersonic transport aircraft