NASA Logo

NTRS

NTRS - NASA Technical Reports Server

Back to Results
The effect of grazing flow on the steady state resistance of square-edged orificesA simple inviscid interaction model has been developed which uses thin airfoil theory to account for pressure forces exerted at the interface between the orifice and grazing flow together with a one-dimensional discharge coefficient concept. The effect of grazing flow boundary layer thickness was also included in the model. Resistance measurements for a wide range of grazing flow speeds and orifice flow rates collapse into a single curve when plotted in terms of effective discharge coefficient versus orifice-to-grazing velocity ratio. The correlation curves for inflow and outflow are different. Data for clustered orifices collapse in the same way as the single orifice. The effect of boundary layer thickness is compared with model predictions. The effect of orifice length-diameter ratio is shown to be significant for inflow but negligible for outflow.
Document ID
19750041690
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Rogers, T.
Hersh, A. S.
(Hersh Acoustical Engineering Chatsworth, Calif., United States)
Date Acquired
August 8, 2013
Publication Date
March 1, 1975
Subject Category
Acoustics
Report/Patent Number
AIAA PAPER 75-493
Meeting Information
Meeting: American Institute of Aeronautics and Astronautics, Aero-Acoustics Conference
Location: Hampton, VA
Start Date: March 24, 1975
End Date: March 26, 1975
Sponsors: American Institute of Aeronautics and Astronautics
Accession Number
75A25762
Distribution Limits
Public
Copyright
Other

Available Downloads

There are no available downloads for this record.
No Preview Available