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Surface pressure measurements in shock wave/boundary-layer interactions

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Abstract

An experimental research program establishing a database of the surface pressure in swept shock wave/boundary-layer interactions is described. An equilibrium turbulent boundary-layer on a flat plate is subjected to impingement by swept planar shock waves genterated by a sharp fin. Various fin angles at 4 different freestream Mach numbers produce a variety of interaction strengths from weak to very strong. For each of different interaction cases, the surface flow patterns are obtained by a kerosene-lampblack-adhesive transparent tape technique. Surface pressures within the interactions are also measured from several streamwise row of taps connected to a computer-controlled Scanivalve system. An extensive error analysis is carried out for the experiments yielding an uncertainty of about ±3%. From these measurements, high spatial resolution surface pressure distributions for different interaction cases are obtained.

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Abbreviations

M :

Mach number

p :

Surface static pressure

R :

Radial distance from fin leading-edge

VCO:

Virtual conical origin

α:

Angle-of-attack of the fin

β:

Angle with respect to incoming free-stream direction, measured from fin leading-edge

pa :

Primary attachment

peak :

Peak value

ps :

Primary separation

ss :

Secondary separation

ui :

Upstream influence

∞:

Incoming freestream

n :

Normal component

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Lee, Y., Garg, S. & Settles, G.S. Surface pressure measurements in shock wave/boundary-layer interactions. KSME International Journal 11, 164–172 (1997). https://doi.org/10.1007/BF02944890

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