Turbulent Boundary-layer Growth Far Downstream in a Slowly Expanding Hypersonic Nozzle PDF Download
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Author: Lu-chung Chang
Publisher:
ISBN:
Category : Aerodynamics, Hypersonic
Languages : en
Pages : 170
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Book Description
Author: Lu-chung Chang
Publisher:
ISBN:
Category : Aerodynamics, Hypersonic
Languages : en
Pages : 170
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Book Description
Author: Arthur Francis Steczkowski
Publisher:
ISBN:
Category : Aerodynamics, Hypersonic
Languages : en
Pages : 106
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Book Description
Author:
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 320
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Book Description
Author: Dennis M. Bushnell
Publisher:
ISBN:
Category : Aerodynamics, Hypersonic
Languages : en
Pages : 44
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Book Description
Turbulent boundary layer measurements on axisymmetric hypersonic nozzle walls.
Author:
Publisher:
ISBN:
Category : Mechanics, Applied
Languages : en
Pages : 814
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Author:
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 514
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Book Description
Author: Arnold Polak
Publisher:
ISBN:
Category : Aerodynamics, Hypersonic
Languages : en
Pages : 56
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Book Description
Results of a study of hypersonic-turbulent boundary-layer separation over axisymmetric bodies are presented. Pressure, heat-transfer and flow visualization data were obtained for a cone-cylinder-flare configuration. The experimental data were correlated with a theoretical prediction. (Author).
Author: R. M. Grabow
Publisher:
ISBN:
Category : Aerodynamics, Hypersonic
Languages : en
Pages : 94
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Book Description
Author: David F. Gates
Publisher:
ISBN:
Category : Supersonic nozzles
Languages : en
Pages : 124
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Book Description
The report describes an experimental study of compressible turbulent boundary layers for which the upstream history was systematically varied. A series of experiments was conducted using both a supersonic half nozzle and a conventional flat plate for which the nozzle throat and flat plate leading edge can be temperature controlled. The supersonic nozzle provided a favorable upstream pressure gradient together with a controlled thermal history at the throat. The flat plate provided upstream temperature control with no pressure history. Velocity and temperature profile and heat-transfer measurements were made in a downstream region of zero-pressure-gradient and constant wall temperature. (Modified author abstract).
Author: Joan Patricia Gosink
Publisher:
ISBN:
Category : Nozzles
Languages : en
Pages : 148
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