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NASA NTRS · 19780061522

Performance characteristics of two annular dump diffusers using suction-stabilized vortex flow control

Abstract

The two diffusers employed in the investigation had the same overall area ratio but different prediffuser area ratios and suction slot geometries. Velocity profile and diffuser pressure recovery performance data were obtained at ambient pressure and temperature, with inlet Mach numbers ranging from 0.18 to 0.41 and suction rate varying from zero to 18% of total inlet mass flow rate. On the basis of the reported investigation it is concluded that suction stabilized vortex flow diffusers show promise for application in combustors because of relatively high static pressure recovery and low total pressure loss obtained in a short length. Performance obtained using a narrow angle (7 degree) prediffuser was superior to that obtained with a prediffuser having a 14 degree included angle.

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BibTeXRIS

Juhasz, A. J., Smith, J. M.. 1978-06-01. Performance characteristics of two annular dump diffusers using suction-stabilized vortex flow control. https://ntrs.nasa.gov/citations/19780061522

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