Experimental and Analytical Investigation of Fast Normal Shock Position Controls for a Mach 2.5 Mixed-compression Inlet PDF Download
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Author: George H. Neiner
Publisher:
ISBN:
Category : Jet engines
Languages : en
Pages : 68
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Book Description
Author: George H. Neiner
Publisher:
ISBN:
Category : Jet engines
Languages : en
Pages : 68
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Author:
Publisher:
ISBN:
Category :
Languages : en
Pages : 304
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Book Description
Author: David N. Bowditch
Publisher:
ISBN:
Category : Aerodynamics, Supersonic
Languages : en
Pages : 40
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Author:
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 104
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Author: Clarence W. Matthews
Publisher:
ISBN:
Category : High-speed aeronautics
Languages : en
Pages : 60
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Book Description
This paper presents an analysis of the ability of a perforated wall in an internal-compression supersonic inlet to control the motion of the shock due to a variety of transients in the flow values at the engine face. The method of one-dimensional unsteady-flow characteristics was used to calculate the shock motion. The perforated walls were found to contain the shock within the inlet for appreciably larger transient magnitudes than was possible with solid walls.
Author:
Publisher:
ISBN:
Category : Aerodynamics
Languages : en
Pages : 866
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Author: United States. National Advisory Committee for Aeronautics
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 860
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Author: Clarence W. Matthews
Publisher:
ISBN:
Category : Automatic control
Languages : en
Pages : 44
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Author: United States. National Aeronautics and Space Administration
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 500
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Author:
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 494
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