Boundary-layer transition and global skin friction measurement with an oil-fringe imaging technique View on Open Library

Boundary-layer transition and global skin friction measurement with an oil-fringe imaging technique

by Daryl J. Monson

No reviews yet
First published: 1993 1 language
Subjects
Skin friction Wind tunnel tests Oils Imaging techniques Boundary layer transition Wind tunnel models Friction measurement Wings

Reviews

Log in or sign up to write a review.

No reviews yet. Be the first!

More by Daryl J. Monson

Attached and separated boundary layers on highly cooled, ablating and nonablating models at M=13.8

Attached and separated boundary layers o...

You Might Also Like

More in Skin friction
Development of in-fiber reflective Bragg gratings as shear stress monitors in aerodynamic facilities

Development of in-fiber reflective Bragg...

Devendra S. Parmar
Skin-friction measurements in a 3-D, supersonic shock-wave/boundary-layer interaction

Skin-friction measurements in a 3-D, sup...

Aerospace Sciences Meeting & Exhibit (32nd 1994 Reno, Nev.)
Flight-measured pressure characteristics of aft-facing steps in high Reynolds number flow at Mach numbers of 2.20, 2.50, and 2.80 and comparison with other data

Flight-measured pressure characteristics...

Sheryll Goecke Powers
Application of Navier-Stokes code PAB3D with k-e turbulence model to attached and separated flows

Application of Navier-Stokes code PAB3D ...

Khaled S. Abdol-Hamid
Shock tunnel studies of scramjet phenomena 1995

Shock tunnel studies of scramjet phenome...

R. G. Morgan
Analytical and numerical investigation of structural response of compliant wall materials

Analytical and numerical investigation o...

R. Balasubramanian