[Skip to Content]
Provided by ASME The American Society of Mechanical Engineers
Banner
Turbo Expo 2026
Allianz MiCo
Milan, Italy

Conference: June 15–19, 2026
Exhibition: June 16–18, 2026
Menu
  • Technical Program
  • Tracks and Organizers
  • Policies
    • Confirm Co-Authorship
    • Presentation Requirements
    • Conflict in Ukraine
    • Code of Conduct/Anti-Harassment
  • Event Site
  • Help/Resources
    • Help Desk Calls
    • Contact Us
    • Organizer Resources
    • Author Resources
      • ASME Plagiarism Screening (iThenticate)
      • ASME Presenter Attendance Policy
      • Turbo Expo Paper Quality Standards
      • ASME Turbo Expo Journal Best Paper Guidelines
      • Conference-Specific Information and Templates
      • Copyright Transfer Form
      • Technical Presentation Tips
      • ​​​​​​​Appeal Process for the Journal of Turbomachinery
      • The Appeal Process for the ASME Journal of Engineering for Gas Turbines and Power Jerzy T. Sawicki, Ph.D., P.E., Editor
      • Indexing
      • Tutorial Handout Template
      • Poster Session Guidelines
      • Authorship and AI Tools
      • Author FAQs
  • Publication Schedule
  • Home
  • Home
  • Turbo Expo 2021 Session Gallery
  • 37-06 Centrifugal Compressor Design
  • Aerodynamic Functional Diagnostics Based on Angular Momentum Transport Lines

59595 - Aerodynamic Functional Diagnostics Based on Angular Momentum Transport Lines 

In analogy with the classical concept of mass-flux-based streamlines, we define Angular Momentum Transport (AMT) lines as an aerodynamic functional diagnostic tool. The AMT lines are lines whose tangents are given by the average angular momentum flux. The mathematical and physical properties of these AMT lines are exploited to study the generation, removal, and transport of angular momentum in turbomachinery components. We illustrate the concept by visualizing AMT lines in two relatively simple flows, namely, vaneless diffuser and von Karman flow (a model of centrifugal compressors). Next, we apply the proposed diagnostic tool to flow in a return channel. A return channel is a part of a multistage centrifugal compressor stage. Its principal function is to remove angular momentum. In this work, we apply the diagnostic tool of AMT lines to a Reynolds averaged Navier Stokes simulation (RANS) and a wall-modeled large eddy simulation (LES) of flow in the return channel.  We show that AMT lines give us insights into the angular momentum transport process that are otherwise not available with conventional visualization tools. In addition, we show that our design of the radial guide vanes has not reached the point where the low fidelity tool of RANS can no longer give us further insight.

Custom JS

double-click to edit, do not edit in source

 

Aerodynamic Functional Diagnostics Based on Angular Momentum Transport Lines

Paper Type

Technical Paper Publication

Description


Session: 37-06 Centrifugal Compressor Design

Paper Number: 59595

Start Time: June 9th, 2021, 09:45 AM

Presenting Author: Xiang Yang

Authors: Xiang Yang Penn State University
Vishal Jariwala Elliott Group
Haosen Xu Pennsylvania State University
Louis Larosiliere Elliott Group

 













 

This site supports all modern browsers, such as Chrome, Firefox, Safari, and Edge. Microsoft no longer supports IE 11 as of August 2021. If you prefer to or you are required to continue using a Microsoft browser, you can use Edge.

  • ASME.ORG
  • Press
  • Terms of Use
  • Privacy Statement
  • ASME Communication Preferences
  • Community Rules

© The American Society of Mechanical Engineers

Stay Connected