NASA Logo

NTRS

NTRS - NASA Technical Reports Server

Back to Results
Skin friction drag measurements by LDVA laser Doppler velocimeter employing a microscope objective as the receiving lens has been developed for measuring fluid velocity inside the boundary layer flow field with a spatial resolution of 40 microns. The method was applied for direct measurement of aerodynamic skin friction drag from the measured velocity gradient at the wall. Experimental results obtained on skin friction and on velocity components in a turbulent boundary layer on a low speed wind tunnel showed good agreement with previously reported data using conventional instruments such as hot-wire anemometers and Preston tubes. The method thus provides a tool for measurement and control of skin friction on aerodynamic bodies without perturbing the flow field.
Document ID
19810060462
Acquisition Source
Legacy CDMS
Document Type
Reprint (Version printed in journal)
Authors
Mazumder, M. K.
(Arkansas Univ. Little Rock, AR, United States)
Wanchoo, S.
(Arkansas Univ. Little Rock, AR, United States)
Mcleod, P. C.
(Arkansas Univ. Little Rock, AR, United States)
Ballard, G. S.
(Arkansas Univ. Little Rock, AR, United States)
Mozumdar, S.
(Arkansas Univ. Little Rock, AR, United States)
Caraballo, N.
(Arkansas, University Little Rock, AR, United States)
Date Acquired
August 11, 2013
Publication Date
August 15, 1981
Publication Information
Publication: Applied Optics
Volume: 20
Subject Category
Instrumentation And Photography
Accession Number
81A44866
Funding Number(s)
CONTRACT_GRANT: NGL-04-001-007
Distribution Limits
Public
Copyright
Other

Available Downloads

There are no available downloads for this record.
No Preview Available