Three-dimensional Flow of Ideal Gas Past Smooth Bodies

Three-dimensional Flow of Ideal Gas Past Smooth Bodies PDF Author: Konstantin Ivanovich Babenko
Publisher:
ISBN:
Category : Aerodynamics
Languages : en
Pages : 532

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Three-dimensional Flow of Ideal Gas Past Smooth Bodies

Three-dimensional Flow of Ideal Gas Past Smooth Bodies PDF Author: Konstantin Ivanovich Babenko
Publisher:
ISBN:
Category : Aerodynamics
Languages : en
Pages : 532

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Book Description


Three-dimensional Flow of Ideal Gas Past Smooth Bodies

Three-dimensional Flow of Ideal Gas Past Smooth Bodies PDF Author: K. I. Babenko
Publisher:
ISBN:
Category : Aerodynamics
Languages : en
Pages :

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Three-dimensional Flow of Ideal Gas Past Smooth Bodies [with List of References]

Three-dimensional Flow of Ideal Gas Past Smooth Bodies [with List of References] PDF Author:
Publisher:
ISBN:
Category : Aerodynamics
Languages : en
Pages : 517

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Three-dimensional Flow of Ideal Gases Around Smooth Bodies

Three-dimensional Flow of Ideal Gases Around Smooth Bodies PDF Author: Konstantin Ivanovich Babenko
Publisher:
ISBN:
Category : Aerodynamics
Languages : en
Pages : 520

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Three-dimensional Flow Ideal Gases Around Smooth Bodies

Three-dimensional Flow Ideal Gases Around Smooth Bodies PDF Author: K. I. Babenko
Publisher:
ISBN:
Category : Gas
Languages : en
Pages :

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The Method of Characteristics for Three-dimensional Real-gas Flows

The Method of Characteristics for Three-dimensional Real-gas Flows PDF Author: Charles R. Strom
Publisher:
ISBN:
Category : Aerodynamics
Languages : en
Pages : 136

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Book Description
The method of characteristics is formulated for the computation of the supersonic flow of an inviscid, reacting gas over a smooth three-dimensional body. Various methods of constructing networks of bicharacteristic lines are examined from the point of view of numerical stability and accuracy. A new method of forming the network, which consists of projecting forward along streamlines from data points on specified data planes, is found to be most easily adopted to the particular requirements of nonequilibrium chemistry. The general method was coded for the IBM 7090 computer and the program demonstrated for the case of an ideal gas. Calculations were made for the case of an ideal gas. Calculations were made for the flow about a spherical-tip 15 degree half-angle cone at 10 degree angle of attack and a generalized elliptical body at zero incidence. Since the program yields the pressure distribution along specified streamlines, it is straightforward, in principle, to link it to a finite-rate chemistry stream tube program to treat three-dimensional, nonequilibrium flows. (Author).

Scientific and Technical Aerospace Reports

Scientific and Technical Aerospace Reports PDF Author:
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 970

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Book Description
Lists citations with abstracts for aerospace related reports obtained from world wide sources and announces documents that have recently been entered into the NASA Scientific and Technical Information Database.

NASA Technical Note

NASA Technical Note PDF Author:
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 478

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The Calculation of Three-dimensional Supersonic Flows Around Spherically-capped Smooth Bodies and Wings: Manual for computer programs

The Calculation of Three-dimensional Supersonic Flows Around Spherically-capped Smooth Bodies and Wings: Manual for computer programs PDF Author: Chong-Wei Chu
Publisher:
ISBN:
Category : Aerodynamics, Supersonic
Languages : en
Pages : 216

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Third Conference on Sonic Boom Research

Third Conference on Sonic Boom Research PDF Author: Ira R. Schwartz
Publisher:
ISBN:
Category : Sonic boom
Languages : en
Pages : 472

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Book Description
Prediction methods for sonic boom generation and propagation with overpressure minimization in supersonic transport design and operation.