Search
Now showing items 1-2 of 2
Numerical Simulation and Parametric Study of a Supersonic Intake
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
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...