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Detection of the transitional layer between laminar and turbulent flow areas on a wing surface (1980)

Hood, W. R.

In: CASI

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Publication Date: 2019-06-27

Description: A system is disclosed for detecting the laminar to turbulent boundary layer transition on a surface while simultaneously taking pressure measurements. The system uses an accelerometer for producing electrical signals proportional to the noise levels along the surface and a transducer for producing electrical signals proportional to pressure along the surface. The signals generated by the accelerometer and transducer are sent to a data reduction system for interpretation and storage.

Keywords: AERODYNAMICS

Format: application/pdf

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