Accession Number : ADA298568
Title : Acquisition and Reduction of Rotor-Tip Static Pressure Transducer Data From a Low Aspect Ratio Transonic Fan.
Descriptive Note : Final rept. Jun 93-Feb 94,
Corporate Author : BATTELLE MEMORIAL INST WRIGHT-PATTERSON AFB OH APPLIED TECHNICAL COMPUTER GR OUP
Personal Author(s) : Russler, Patrick M.
PDF Url : ADA298568
Report Date : FEB 1995
Pagination or Media Count : 37
Abstract : This report details the acquisition and reduction of Over-The-Rotor (OTR) static pressure data. These data were acquired during the Augmented Damping of Low Aspect Ratio Fans (ADLARF) test conducted at the Compressor Research Facility (CRF). The CRF is located at Wright Laboratory on Wright-Patterson A.F.B. in Ohio. The CRF is one of two high-speed compressor test facilities at Wright Laboratory. The report is primarily concerned with the acquisition and reduction of the OTR data, and is intended to demonstrate the ability to reduce, display, and analyze static pressure data acquired from the tip region of fans and compressors. The ability to show basic shock structure in the tip region of a transonic fan is clearly demonstrated. Problems associated with the acquisition and reduction process are also addressed. Although these data were originally intended only to demonstrate proof of concept, they have also provided valuable insight concerning the tip flow region of the ADLARF fan. (AN)
Descriptors : *SHOCK WAVES, *GAS TURBINES, *STATIC PRESSURE, *AXIAL FLOW COMPRESSORS, VELOCITY, STEADY STATE, AIRCRAFT ENGINES, PRESSURE TRANSDUCERS, STATIC LOADS, AIR FLOW, DAMPING, VORTICES, PRESSURE MEASUREMENT, MASS FLOW, FLOW FIELDS, DATA REDUCTION, DATA ACQUISITION, FANS, CALIBRATION, ASPECT RATIO, TRANSONIC FLOW, AXIAL FLOW, COMPRESSOR ROTORS, BLADE TIPS.
Subject Categories : Fluid Mechanics
Jet and Gas Turbine Engines
Distribution Statement : APPROVED FOR PUBLIC RELEASE