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نمایش تعداد 1-2 از 2
Numerical Simulation and Parametric Study of a Supersonic Intake
سال: 2013
خلاصه:
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
سال: 2014
خلاصه:
.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...