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نمایش تعداد 1-7 از 7
Supersonic inlet buzz detection using pressure measurement on wind tunnel wall
Feasibility of an innovative buzz detection technique through measuring the static pressure
outside a mixed-compression supersonic inlet is studied. The buzz is an instability
phenomenon that occurs almost in all ...
Novel Method for Supersonic Inlet Buzz Measurement in Wind Tunnel
A method for detection of buzz from wall sensors has been proposed.
AXISYMMETRIC AND THREE-DIMENSIONAL FLOW SIMULATION OF A MIXED COMPRESSION SUPERSONIC AIR INTAKE
. 3D
effects in axisymmetric supersonic intakes in axisymmetric
flow condition are not enough strong to affect significantly on
the intake performance in all operational condition. However, it
seems that these effects play a...
Effects of Boundary-Layer Bleed Parameters on Supersonic Intake Performance
The performance and the buzz onset of a supersonic mixed-compression axisymmetric intake are xperimentally investigated. Effects of the slot bleed position, angle, and width on the intake performance and on the buzz ...
Investigation of Corner Rounding Effects on the Performance of a Supersonic Air Intake
In this research, flow is simulated numerically through and around a mixed-compression intake to investigate effects of corner rounding on intake performance at free stream Mach numbers of 1.8, 2 and 2.2 and at zero degrees ...
Numerical Simulation and Parametric Study of a Supersonic Intake
A computational fluid dynamics code was developed to compute the flow inside and around a supersonic external compression axisymmetric intake. The code solves the Reynolds-averaged Navier–Stokes equations using an explicit ...
Performance Investigation of a Supersonic Air Intake in the Presence of the Boundary Layer Suction
The performance of a supersonic mixed compression air intake has been investigated experimentally. The intake is of axisymmetric one and has been designed for a free stream Mach number of 2.0. The present work has two main ...