Aero-Thermal Flow Analysis
Pressure contours and velocity vectors for flow through first stage blades are determined from computational fluid dynamics codes. Boundary element codes determine heat transfer coefficients that are then used in thermal and stress analysis of the blades.
Turbo-compressor test facility being prepared for full speed test of performance near stall and surge conditions.
Contours of pressure on the mid-width plane in the vaneless diffuser. Images displayed at 10-ms intervals.
Fluid dynamics, heat transfer, combustion, and fluid-structure interaction are essential disciplines to the effective design, application, and performance evaluation of gas turbines. Southwest Research Institute (SwRI) maintains a variety of commercial and SwRI-developed analysis and computational codes to meet specific needs. A number of flow facilities are used in conjunction with computational methods to support simulation and understanding of fluid flows and their interactions with structures. Flow visualization techniques enhance this capability.
Flow facilities include:
- High pressure (2,500 psi), large volume (980 ft3) N2 gas blowdown system
- Low pressure (2 to 200 psia) air and inert gas recirculating loop to 8 MMSCFD
- Low pressure (to 200 psia) natural gas recirculating loop (to 6 MMSCFD)
- High pressure (to 1,400 psi) natural gas recirculating loop (to 165 MMSCFD)
- 0-6,000 gpm low-turbulence water tunnel
- High-pressure, high-flow combustion tunnel
Turbomachinery Test Facility
Our turbomachinery laboratory is set up to conduct detailed research on centrifugal compressors, gas turbines, internal flows, performance, and the onset of problems such as stall, surge, and various shaft and bearing instabilities. Special instrumentation including laser measurements and high-G self-power imbedded telemetry systems for instrument signals are developed and used by SwRI.
SwRI uses computation fluid dynamics, along with other analysis and 1D modeling, to predict turbine flows, local behaviors, contributions to performance, and the onset of stall, surge, flutter, or other instabilities. Blade temperature predictions can be made with various degrees and types of cooling as a diagnostic prediction or as a guide to interpreting measurements.
More information about aero-thermal turnkey design services and fault diagnostics offered at SwRI is available in this printable PDF flyer.
SwRI can offer you a full range of capabilities and experience in rotating machinery technologies including becoming an extension of your engineering department. Contact us for more information about rotating machinery technologies, or how you can contract with SwRI.