0

Measurement of Swirling Flow Field Using the Single Slanted Hot-Wire Technique FREE

[+] Author Affiliations
H. W. Shin

Massachusetts Institute of Technology

Z. A. Hu

Beijing Institute of Aeronautics & Astronautics

Paper No. 85-IGT-76, pp. V001T02A028; 6 pages
doi:10.1115/85-IGT-76
From:
  • ASME 1985 Beijing International Gas Turbine Symposium and Exposition
  • Volume 1: Aircraft Engine; Turbomachinery
  • Beijing, People’s Republic of China, September 1–7, 1985
  • Conference Sponsors: International Gas Turbine Institute
  • ISBN: 978-0-7918-7942-9
  • Copyright © 1985 by ASME

abstract

This paper presents the use of a single slanted hot wire to measure the three velocity components of a swirling flow field. In its usage, the hot wire probe has been calibrated in a subsonic air jet for both speed and direction. It was then used to measure the swirling flow field associated with the presence of an inlet model. Using Hybrid Method, the final velocity components are obtained via the solution of a set of simultaneous nonlinear equations given the voltage readings at three orientations of the hot wire probe at a point in the flow field. The distortions of total pressure and velooity were also measured in the same inlet model.

Copyright © 1985 by ASME
Topics: Wire , Swirling flow
This article is only available in the PDF format.

Figures

Tables

Interactive Graphics

Video

Country-Specific Mortality and Growth Failure in Infancy and Yound Children and Association With Material Stature

Use interactive graphics and maps to view and sort country-specific infant and early dhildhood mortality and growth failure data and their association with maternal

NOTE:
Citing articles are presented as examples only. In non-demo SCM6 implementation, integration with CrossRef’s "Cited By" API will populate this tab (http://www.crossref.org/citedby.html).

Some tools below are only available to our subscribers or users with an online account.

Related Content

Customize your page view by dragging and repositioning the boxes below.

Related eBook Content
Topic Collections

Sorry! You do not have access to this content. For assistance or to subscribe, please contact us:

  • TELEPHONE: 1-800-843-2763 (Toll-free in the USA)
  • EMAIL: asmedigitalcollection@asme.org
Sign In