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Predicting Transition from Laminar to Turbulent Flow over a SurfaceA prediction of whether a point on a computer-generated surface is adjacent to laminar or turbulent flow is made using a transition prediction technique. A plurality of instability modes are obtained, each defined by one or more mode parameters. A vector of regressor weights is obtained for the known instability growth rates in a training dataset. For an instability mode in the plurality of instability modes, a covariance vector is determined. A predicted local instability growth rate at the point is determined using the covariance vector and the vector of regressor weights. Based on the predicted local instability growth rate, an n-factor envelope at the point is determined.
Document ID
20160011052
Acquisition Source
Langley Research Center
Document Type
Other - Patent
Authors
Rajnarayan, Dev
Sturdza, Peter
Date Acquired
September 6, 2016
Publication Date
August 16, 2016
Subject Category
Aerodynamics
Fluid Mechanics And Thermodynamics
Report/Patent Number
Patent Application Number: US-Patent-Appl-SN-14/019,448
Patent Number: US-Patent-9,418,202
Funding Number(s)
CONTRACT_GRANT: NNL08AA08C
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Patent
US-Patent-9,418,202
Patent Application
US-Patent-Appl-SN-14/019,448
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