Further development of a Dual-Probe Digital Sampling (DPDS) technique for measuring flow fields in rotating machines
Loading...
Authors
Neuhoff, F.
Advisors
Second Readers
Subjects
Compressor Measurements
High Response Probes
Turbomachinery Flow Fields
High Response Probes
Turbomachinery Flow Fields
Date of Issue
1982-09
Date
1982-09
Publisher
Monterey, California. Naval Postgraduate School
Language
Abstract
Following a review of the technique, detailed descriptions are given of
the procedures developed for calibrating and applying a system of two simple
semi-conductor (Kulite) pressure probes to measure the velocity field from a
high speed rotor. Calibration tests of a "second generation1
' probe set in a
steady free jet, procedures for deriving calibration equations and subsequent
verification tests are described in turn. Data reduction procedures and
software involved in the application of the probe system with controlled digital data sampling, to obtain the blade-to-blade velocity field in a
machine are documented with examples of results. Successes and potential
problems are evaluated.
Type
Technical Report
Description
Final Report. Principal Investigator, Dr. R. P. Shreeve, Turbopropulsion Laboratory, Code 67Sf, Naval Postgraduate School, Monterey, CA 93943.
Series/Report No
Department
Organization
Identifiers
NPS Report Number
NPS67-82-01CR
Sponsors
Funding
N00CUi-79-C-0088
Format
Citation
Distribution Statement
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.
