Experiments with Biconvex Aerof 6 ils in Low - Density , and Double - Wedge Supersonic Flow
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Determination of Shock Standoff Distance for Wedge at Supersonic Flow
An experimental investigation is conducted to calculate the shock standoff (SSO) distance in front of an acute-angled wedge. For this experimentation, simple water flows channel analysis is carried out. The flow velocity is varied from 13.2 cm/s to 25.5 cm/s increasing in steps of 1 cm/s. A velocity of 13.2 cm/s corresponds to Froude number 1.13 and velocity of 25.5 cm/s to Froude number 1.41. ...
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تاریخ انتشار 1968