Robbert Pannekeet

Design, Validation and Application of a Radial Cascade for Centrifugal Compressors

A novel sector test rig has been used to evaluate a new airfoil concept for multistage radial compressors. The test rig is supported by a blow-down facility where the operation conditions are adjusted by controlling mass flow, pressure and temperature. At inlet to the sector test rig itself a set of adjustable inlet guide vanes provide the test vanes with the correct inlet three-dimensional flow-field. The rig is equipped with instrumentation to allow a detailed description of the inlet and outlet conditions, as well as the blade pressure loading. This rig, using rapid prototyped vanes, allows design candidates to be screened quickly and is ideal for conducting an experimental investigation of a design space using a Design-of-Experiments approach. In this paper the rationale for the sector approach is described, the design of the test rig with 3D-CFD methods is outlined and a detailed validation of the rig is presented. For the vane in question detailed investigations of different operation points close to stall are reported, blade pressures and inlet and exit flow profiles are given. Where applicable, measurement data from the sector rig was compared to 3D-CFD calculations of the full annulus multistage configuration, to 3D-CFD calculations of the sector rig itself and to the test results from a 1.5-stage rotating test rig. The measurement data are compared to the CFD predictions and served as a calibration basis for the design tools.Copyright

Experimental Test Results for a Fiber Bragg Grating-based Flow Sensor:

A fiber optic-based mass flow sensor has been developed that uses fiber Bragg gratings to deduce flow velocity. Flow velocity, local temperature, pressure measurements (which all can be extracted using fiber Bragg gratings), and geometric information can be combined to determine mass flow. A range of concepts have each been investigated and compared using the same “design of experiment” for each sensor. The most promising concept has been further developed into a prototype. The working prototype successfully demonstrated a thermally insensitive sensor design that has the capability to track flow velocities. The sensor design is incorporated directly with a structural beam element to magnify the strain effect while simultaneously compensating for thermally induced wavelength shifts in the sensor response. Further testing has been performed using three flexible beams at different angular positions, demonstrating that flow angles can be measured using a similar approach to that used for three-hole pneumatic probes. As a final test, the sensor has been tested in a shock tube, demonstrating superior performance to steady pneumatic measurements, which rely on tubing to reach the measurement location.

Experimental Test Results for a Fiber Bragg Grating-Based Flow Sensor

A fiber optic-based mass flow sensor has been developed that uses fiber Bragg gratings to deduce flow velocity. Flow velocity, local temperature, pressure measurements (that all can be extracted using fiber Bragg gratings) and geometric information can be combined to determine mass flow. A range of concepts have been investigated and compared using the same “design of experiment” for each sensor. The most promising concept has been further developed into a prototype. The working prototype successfully demonstrated a thermally insensitive sensor design that has the capability to track flow velocities. The sensor design is incorporated directly with a structural beam element to magnify the strain effect while simultaneously compensating for thermally-induced wavelength shifts in the sensor response. Further testing has been performed using three flexible beams at different angular positions showing that flow angles can be measured similar to the approach used for 3-hole pneumatic probes. As a final test, the sensor has been tested in a shock tube demonstrating superior performance compared to steady pneumatic measurements which rely on tubing to reach the measurement location.Copyright