Naval Postgraduate School
Report of tests of a compressor configuration of DCA blading.
reportoftestsofc00hime.pdf (9.118Mb)Abstract
Results of an experimental program to measure the performance
of a compressor stator cascade consisting of 20
DCA blades of chord 5.01 inches, aspect ratio 2.0 and solidity
1.67 under conditions of varying incidence angle and
Reynolds number are reported. Flow quality and blade performance
data were obtained using pneumatic probe surveys
and surface pressure measurements. Changes in Reynolds
number in the range of 500,000 to 770,000 did not measurably
effect either flow quality or blade performance. Changes
in incidence angle over the range -15 to 10 degrees produced
generally well behaved blade performance parameters.
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