Velocity Measurements in a 3D Shock Wave Laminar Boundary Layer Interaction. Part 1. Low Speed 2D LDV Measurements

Velocity Measurements in a 3D Shock Wave Laminar Boundary Layer Interaction. Part 1. Low Speed 2D LDV Measurements
Author: G. Degrez
Publisher:
Total Pages: 34
Release: 1984
Genre:
ISBN:


Download Velocity Measurements in a 3D Shock Wave Laminar Boundary Layer Interaction. Part 1. Low Speed 2D LDV Measurements Book in PDF, Epub and Kindle

Single component LDV (Laser Doppler Velocimetry) measurements were obtained in the separated 2D thin laminar boundary layer over an elliptic cylinder. The ellipse had an axis ratio of 4:1 and the incoming Reynolds numbers based on the minor axis were 675 and 1350. Velocity measurements were obtained within 0.05 mm from the surface both in attached and reverse flow regions. Painting the model with matt black paint and covering the tunnel walls proved to be effective means of improving signal quality. Measurements were successful both in back and forward scatter modes. The velocity profiles measured with Bragg cells indicate that the flow is separated at the ellipse mid-chord and that the separation bubble extends far downstream in the wake. The velocity profiles in the attached flow region compare well with the results of a boundary layer computation.


Velocity Measurements in a 3D Shock Wave Laminar Boundary Layer Interaction. Part 1. Low Speed 2D LDV Measurements
Language: en
Pages: 34
Authors: G. Degrez
Categories:
Type: BOOK - Published: 1984 - Publisher:

GET EBOOK

Single component LDV (Laser Doppler Velocimetry) measurements were obtained in the separated 2D thin laminar boundary layer over an elliptic cylinder. The ellip
Scientific and Technical Aerospace Reports
Language: en
Pages: 836
Authors:
Categories: Aeronautics
Type: BOOK - Published: 1994 - Publisher:

GET EBOOK

Velocity Measurements in a 3D (Three Dimensional) Shock Wave Laminar Boundary Layer Interaction
Language: en
Pages: 46
Authors: G. Degrez
Categories:
Type: BOOK - Published: 1987 - Publisher:

GET EBOOK

An experimental investigation of the three dimensional laminar boundary layer separation associated with an incident swept shock wave was conducted in the von K
Proceedings
Language: en
Pages: 638
Authors: International Council of the Aeronautical Sciences
Categories: Aeronautics
Type: BOOK - Published: 1984 - Publisher:

GET EBOOK

Aeronautical Engineering
Language: en
Pages: 538
Authors:
Categories: Aeronautics
Type: BOOK - Published: 1991 - Publisher:

GET EBOOK