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The correlation coefficients of pressure at different chordwise locations around a square prism are also calculated.
Experimental studies on drag reduction of a square prism were conducted.
An experimental PIV study is presented that addresses the confined 3D laminar flow behaviour past a square prism.
Second, the aerodynamic vibration of a square prism is simulated using a multi-degree-of-freedom model with base isolation.
To control the flow around a square prism, a small rod was set upstream of the prism.
Effectiveness of the approach in suppressing the aerodynamic instabilities of a square prism was confirmed in earlier studies by the authors.
Similar(38)
Figure 2 shows three of the many possible orientations that a uniform square prism might adopt when floating, with half its volume submerged in a liquid for which ρ = 2ρ′; they are separated by rotations of 22.5°.
Encyclopædia Britannica, Inc. Figure 2: Three possible orientations of a uniform square prism floating in liquid of twice its density.
A new digital pressure scanning system has been developed and used to obtain pressure data on a 2D square prism with leading edge flaps.
This paper presents and discusses the results of wind tunnel measurements of the pressure distributions on the lateral sides of a 2D square prism with vibrating leading edge flaps.
Chaotic motion of a harmonically excited square prism modelled as a Duffing oscillator and kept in fluid flow is considered.
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