NASA Logo

NTRS

NTRS - NASA Technical Reports Server

Back to Results
The obstacle block as a device to measure turbulent skin friction in compressible flowThe obstacle block, developed as an alternative to the Preston tube for indirectly measuring skin friction on smooth surfaces in incompressible flows, is examined as a device for compressible flows as well. The block, which is congruent with a surface static pressure orifice, has a geometry which is easily specified and thus has a universal calibration. Data from two independent studies are used to establish such a calibration using 'wall' variables, valid for Mach numbers up to about 3. Various aspects concerning practical application of the device are examined, such as sensitivity to yaw and the minimum permissible axial spacing between blocks. Several examples showing the utility of the device are given.
Document ID
19820041129
Acquisition Source
Legacy CDMS
Document Type
Conference Proceedings
Authors
Elfstrom, G. M.
(National Aeronautical Establishment High Speed Aero Laboratory, Ottawa, Canada)
Kostopoulos, C.
(National Aeronautical Establishment Ottawa Ontario, Canada)
Peake, D. J.
(NASA Ames Research Center Moffett Field, CA, United States)
Fisher, D. F.
(NASA Flight Research Center Edwards, CA, United States)
Date Acquired
August 10, 2013
Publication Date
January 1, 1982
Subject Category
Instrumentation And Photography
Report/Patent Number
AIAA PAPER 82-0589
Meeting Information
Meeting: In: Aerodynamic Testing Conference
Location: Williamsburg, VA
Start Date: March 22, 1982
End Date: March 24, 1982
Accession Number
82A24664
Distribution Limits
Public
Copyright
Other

Available Downloads

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