Abstract
This paper investigates experimentally the development of the viscous sublayer in a two-dimensional incompressible turbulent wall boundary layer under severe pressure gradients. The wall was also moderately heated and the influence of heat transfer on the development of the viscous sublayer was included. A semi-empirical equation for the thickness of the viscous sublayer: $$\delta _s = 11.5\frac{\nu }{{U_\tau }}(0.61\frac{{T_\omega }}{{T_s }})^{1/2}$$ was derived, which holds everywhere except closely near the separation point of the boundary layer. The measurements were made on a flat plate in a test section 1.7 m long and 0.8 m wide. The height and shape of the top surface of the test section could be varied, and thus it was possible to imposed different pressure gradients on the flow. Specially designed fine probes facilitated the measurement of the velocity distribution very close to the wall.
Sign-in/Register to access full text options 
Talk to us
Join us for a 30 min session where you can share your feedback and ask us any queries you have
Schedule a callDisclaimer: All third-party content on this website/platform is and will remain the property of their respective owners and is provided on "as is" basis without any warranties, express or implied. Use of third-party content does not indicate any affiliation, sponsorship with or endorsement by them. Any references to third-party content is to identify the corresponding services and shall be considered fair use under The CopyrightLaw.
