Axial Machines Archive

Axial Machines Files

CHT Assessment of a 3-D Vane with Cooling and Comparison to Experiments

Updated on 29 December 2016

  • The High Impact Technologies (HIT) Research Turbine Vane at the U.S. Air Force Research Laboratory is a three-dimensional, fully film-cooled modern turbine inlet vane. In this paper, Captain Jamie Johnson and Paul King from the Air Force Institute of Tec

Highly Loaded Low-Pressure Turbine: Design, Numerical and Experimental Analysis

Updated on 25 April 2017

  • From the Journal of Propulsion and Power, a paper describing the design of a low pressure turbine at the US Air Force Research Lab as well as numerical and experimental analysis. ADS CFD analysis of the LPT was done using ADS Code LEO.

Implicit Scaling Case Study

Updated on 29 December 2016

  • A study comparing the effectiveness of scaled unsteady simulations to full wheel unsteady simulations. A description of ADS' implicit scaling method for reducing the start up cost of scaled unsteady simulations.

Non-Axisymmetric Endwall Contouring of Front Loaded High-Lift Low Pressure Turbines

Updated on 22 January 2018

  • This paper will detail a non-axisymmetric endwall contour design for a front loaded high lift research profile.

PSU ME 597 - Effect of Vortex Distribution on Aerodynamic 3D Design of High Pressure Turbine Vanes and Blades

Updated on 25 January 2018

  • PSU ME 597 - Effect of Vortex Distribution on Aerodynamic 3D Design of High Pressure Turbine Vanes and Blades

PSU ME 597 - Impact of Swirl Distribution of Stage 6 of the NASA E3 Compressor

Updated on 22 January 2018

  • PSU ME 597 - Impact of Swirl Distribution of Stage 6 of the NASA E3 Compressor

PSU ME 597 - NASA E3 Stage 1 Turbine Study on Tip Clearance and Facility Scaling

Updated on 22 January 2018

  • PSU ME 597 - NASA E3 Stage 1 Turbine Study on Tip Clearance and Facility Scaling

Rotor 67 Analysis using ADS CFD

Updated on 29 December 2016

  • ADS CFD is used to analyze Rotor 67. A transonic rotor

Stage 35 Analysis with ADS CFD

Updated on 29 December 2016

  • NASA Stage 35 is analyzed using ADS CFD.

Unsteady Aerodynamic Interaction in a Closely Coupled Turbine Consistent with Contra-Rotation

Updated on 21 February 2017

  • A contra-rotating turbine is analyzed using unsteady CFD analysis and compared against experimental data.