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 SOUTHWEST RESEARCH INSTITUTE

Rotating Machinery Technologies

Aero-Thermal Flow Analysis

 

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  Image of pressure contours and velocity vectors
 

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.

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.

Flow Instability

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.

 

image of aero-thermal test facility   image of contours of pressure on the mid-width plane in the vaneless diffuser. Images displayed at 10-ms intervals.

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.

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. For more information about rotating machinery technologies, or how you can contract with SwRI, please contact Klaus Brun, Ph.D., at kbrun@swri.org or (210) 522-5449.

 

machinery.swri.org

 

Contact Information

Klaus Brun, Ph.D.

Gas Turbine Technology

(210) 522-5449

kbrun@swri.org

machinery.swri.org

Related Terminology

rotordynamics

aero-thermal flow

fluid dynamics

flow instability

flow measurement

turbomachinery test facility

flow visualization techniques

gas turbines

Related Web Sites

IGTI

PRCI

WTUI

Gas/Electric Partnership

Related SwRI Links

Fluids and Machinery Engineering Department

Mechanical Engineering Division

| Fluids and Machinery Engineering Department | Mechanical Engineering Division | SwRI Home |

Southwest Research Institute® (SwRI®), headquartered in San Antonio, Texas, is a multidisciplinary, independent, nonprofit, applied engineering and physical sciences research and development organization with 11 technical divisions.

January 03, 2013