Report of tests of a compressor configuration of DCA blading.
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Authors
Himes, Stephen J.
Subjects
cascade
DCA blading
DCA blading
Advisors
Shreeve, Raymond P.
Date of Issue
1983-06
Date
June 1983
Publisher
Monterey, California. Naval Postgraduate School
Language
en_US
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.
Type
Thesis
Description
Series/Report No
Department
Aeronautics
Organization
Naval Postgraduate School (U.S.)
Identifiers
NPS Report Number
Sponsors
Funding
NA
Format
Citation
Distribution Statement
Approved for public release; distribution is unlimited.
Rights
This publication is a work of the U.S. Government as defined in Title 17, United States Code, Section 101. Copyright protection is not available for this work in the United States.