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    Numerical Simulation and Parametric Study of a Supersonic Intake 

    Type: Journal Paper
    Author : M.R.Soltani; جواد سپاهی یونسی; M Farahani; A. Maseud; Javad Sepahi-Younsi
    Year: 2013
    Abstract:

    flow ratio, flow distortion, and drag coefficient of the intake were then numerically investigated. The results showed that when the spike deflection angle of the intake was changed from 28° (designed base case) to 30°, the intake drag coefficient...

    Performance Investigation of a Supersonic Air Intake in the Presence of the Boundary Layer Suction 

    Type: Journal Paper
    Author : Mohammd Reza Soltani; جواد سپاهی یونسی; A Daliri; Javad Sepahi-Younsi
    Year: 2014
    Abstract:

    .2 and at zero degrees angle of attack. Total pressure recovery, mass flow ratio, and flow distortion have been selected to assess the intake performance. The bleed slot is located upstream of the intake throat

    perpendicular to the compression ramp surface...

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