0
Research Papers

An Analysis of Axial Compressor Cascade Aerodynamics: Part I—Potential Flow Analysis With Complete Solutions for Symmetrically Cambered Airfoil Families

[+] Author and Article Information
G. L. Mellor

Princeton University, Princeton, N. J.

J. Basic Eng 81(3), 362-377 (Sep 01, 1959) (16 pages) doi:10.1115/1.4008477 History: Received August 05, 1958; Published September 01, 1959; Online February 20, 2019

Abstract

A method is presented whereby complete potential flow solutions for any cascade geometry may be obtained with comparatively great rapidity on desk calculators. This solution is carried out for the case of symmetrically cambered airfoils such as the 65-series compressor and circular are airfoils and the results presented in a compact graphical form completely account for the potential flow effects of camber, profile, thickness, stagger, solidity, and angle of attack. Real fluid effects will be assessed and correlated in Part II using the present results as a supporting theory.

Copyright © 1959 by ASME
Your Session has timed out. Please sign back in to continue.

References

Figures

Tables

Errata

Related

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 Journal Articles
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