Accession Number : AD0714585
Title : Aerodynamic Design of Symmetrical Blading for Three-Stage Axial Flow Compressor Test Rig.
Descriptive Note : Technical rept.,
Corporate Author : NAVAL POSTGRADUATE SCHOOL MONTEREY CALIF
Personal Author(s) : Vavra,Michael H.
Report Date : 01 SEP 1970
Pagination or Media Count : 62
Abstract : The report deals with the aerodynamic design of an axial compressor stage with symmetrical bladings for a research program to investigate tip clearance effects in a three-stage compressor. It establishes the blading data and the stage performance with an iterative three-dimensional approach, and gives criteria for the drive and the flow measuring device of the test unit. The calculated distributions of the flow properties in the stage will be used for future comparisons with test data. (Author)
Descriptors : (*TEST EQUIPMENT, AXIAL FLOW COMPRESSOR BLADES), (*AXIAL FLOW COMPRESSOR BLADES, DESIGN), AERODYNAMIC CHARACTERISTICS, THREE DIMENSIONAL FLOW
Subject Categories : Hydraulic and Pneumatic Equipment
Test Facilities, Equipment and Methods
Distribution Statement : APPROVED FOR PUBLIC RELEASE