Contribution to the Study of Gap Induced Boundary Layer Transition in Hypersonic Flow PDF Download
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Author: J. M. Charbonnier
Publisher:
ISBN:
Category :
Languages : en
Pages :
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Author: J. M. Charbonnier
Publisher:
ISBN:
Category :
Languages : en
Pages :
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Author: Sandy Tirtey
Publisher: LAP Lambert Academic Publishing
ISBN: 9783843353243
Category :
Languages : en
Pages : 240
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Book Description
Roughness induced boundary layer transition has been one of the main research topics for the hypersonic community over the last half- century. The major interest into the understanding of this phenomenon relies in the key role played by transition prediction methods on hypersonic vehicles thermal protection system (TPS) design. Several boundary layer transition predictions methods have been developed but a review of these transition criteria reveals a lack a physics associated with these engineering methods together with a lack of reliable flight data. The work presented in this thesis is a first step trying to fill this gap. First, the physical mechanisms associated with hypersonic roughness induced transition are investigated both experimentally and numerically. Secondly, an hypersonic roughness induced transition experiment has been developed for the EXPERT mission, aiming to obtain high quality flight data.
Author: Kenneth F. Stetson
Publisher:
ISBN:
Category : Aerodynamics, Hypersonic
Languages : en
Pages : 116
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This is a survey paper on the subject of hypersonic boundary-layer transition. Part 1 discusses boundary-layer stability theory, hypersonic boundary-layer stability experiments, and a comparison between theory and experiment. Part 2 contains comments on how many configuration and flow parameters influence transition. Part 3 discusses some additional general aspects of transition. Part 4 discusses problems of predicting transition and comments on three prediction methods. Part 5 contains some general guidelines for prediction methodology. Keywords: Boundary layer transition, Boundary layer stability, Hypersonic boundary layers.
Author: Michael Hodge McCloskey
Publisher:
ISBN:
Category : Boundary layer
Languages : en
Pages : 662
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Author:
Publisher:
ISBN:
Category : Aerodynamics, Hypersonic
Languages : en
Pages : 28
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Author: C. J. Stalmach
Publisher:
ISBN:
Category :
Languages : en
Pages : 77
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Author: Francesco Avallone
Publisher: Youcanprint
ISBN: 8891187836
Category : Technology & Engineering
Languages : en
Pages : 189
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The application of non-intrusive experimental techniques is a break-through in the comprehension of the physical mechanisms governing roughness-induced transition in hypersonic flows. In this thesis, IR Thermography, Planar and Tomographic Particle Image Velocimetry are applied. They show a great potentiality in quantifying the most relevant flow features upstream and downstream of three-dimensional roughness elements. Particularly, non-intrusive measurements of the two-dimensional and three-dimensional velocity flow fields are reported and discussed.
Author:
Publisher:
ISBN:
Category : Aerodynamics, Hypersonic
Languages : en
Pages : 92
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Author: John Benjamin Anders
Publisher:
ISBN:
Category : Boundary layer control
Languages : en
Pages : 36
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Author: Gary T. Chapman
Publisher:
ISBN:
Category : Fluid mechanics
Languages : en
Pages : 38
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