Publication Date:
2019-07-13
Description:
A nonintrusive skin-friction meter has been found useful for a variety of complex wind-tunnel flows. This meter measures skin friction with a remotely located laser interferometer that monitors the thickness change of a thin oil film. Its accuracy has been proven in a low-speed flat-plate flow. The wind-tunnel flows described here include sub-sonic separated and reattached flow over a rearward-facing step, supersonic flow over a flat plate at high Reynolds numbers, and supersonic three - dimensional vortical flow over the lee of a delta wing at angle of attack. The data-reduction analysis was extended to apply to three-dimensional flows with unknown flow direction, large pressure and shear gradients, and large oil viscosity changes with time. The skin friction measurements were verified, where possible, with results from more conventional techniques and also from theoretical computations.
Keywords:
Lasers and Masers
Type:
NASA/TM-81-207537
,
NAS 1.15:207537
,
IEEE-Publ-81CH1712-9
,
ICIASF 1981; 232-243|International Congress on Instrumentation in Aerospace Simulation Facilities; Sep 30, 1981; Dayton, OH; United States
Format:
application/pdf
