0
TECHNICAL PAPERS

A Navier–Stokes Analysis of the Stall Flutter Characteristics of the Buffum Cascade

[+] Author and Article Information
Stefan Weber

Max F. Platzer

Department of Aeronautics and Astronautics, Naval Postgraduate School, Monterey, CA 93943-5000

J. Turbomach 122(4), 769-776 (Feb 01, 2000) (8 pages) doi:10.1115/1.1312800 History: Received February 01, 2000
Copyright © 2000 by ASME
Your Session has timed out. Please sign back in to continue.

References

Figures

Grahic Jump Location
O-type 241×61 point grid for the Buffum cascade
Grahic Jump Location
Steady-state pressure distribution, M=0.5,α=61.1 deg,Re=0.9×106
Grahic Jump Location
Steady-state pressure distribution at leading edge, M=0.5,α=61.1 deg,Re=0.9×106
Grahic Jump Location
Steady-state velocity vectors at leading edge, M=0.5,α=61.1 deg,Re=0.9×106
Grahic Jump Location
Real part of unsteady pressure distribution at low incidence, k=1.2,Φ=180 deg,M=0.5,Re=0.9×106
Grahic Jump Location
Imaginary part of unsteady pressure distribution at low incidence, k=1.2,Φ=180 deg,M=0.5,Re=0.9×106
Grahic Jump Location
Local stability analysis at low incidence, k=1.2,Φ=180 deg,M=0.5,Re=0.9×106
Grahic Jump Location
Local stability analysis at low incidence, k=0.8,Φ=180 deg,M=0.5,Re=0.9×106
Grahic Jump Location
Predicted pitching moment coefficient at low incidence, Φ=180 deg,M=0.5,Re=0.9×106
Grahic Jump Location
Steady-state pressure distribution, M=0.5,α=67.2 deg,Re=0.9×106
Grahic Jump Location
Steady-state Mach number contours, M=0.5,α=67.2 deg,Re=0.9×106
Grahic Jump Location
Real part of unsteady pressure distribution at high incidence, k=1.2,Φ=180 deg,M=0.5,Re=0.9×106
Grahic Jump Location
Imaginary part of unsteady pressure distribution at high incidence, k=1.2,Φ=180 deg,M=0.5,Re=0.9×106
Grahic Jump Location
Predicted unsteady Mach number contours at high incidence, k=1.2,Φ=180 deg,M=0.5,Re=0.9×106
Grahic Jump Location
Local stability analysis at high incidence, k=1.2,Φ=180 deg,M=0.5,Re=0.9×106
Grahic Jump Location
Local stability analysis at high incidence, k=0.8,Φ=180 deg,M=0.5,Re=0.9×106
Grahic Jump Location
Local stability analysis at high incidence, k=0.4,Φ=180 deg,M=0.5,Re=0.9×106
Grahic Jump Location
Predicted unsteady aerodynamic moment coefficient at high incidence, Φ=180 deg,M=0.5,Re=0.9×106

Tables

Errata

Discussions

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