0
TECHNICAL PAPERS

On Flowfield Periodicity in the NASA Transonic Flutter Cascade

[+] Author and Article Information
J. Lepicovsky

QSS Group, Inc., Cleveland, OH 44135

R. V. Chima, E. R. McFarland, J. R. Wood

NASA Glenn Research Center, Cleveland, OH 44135

J. Turbomach 123(3), 501-509 (Feb 01, 2000) (9 pages) doi:10.1115/1.1378300 History: Received February 01, 2000
Copyright © 2001 by ASME
Your Session has timed out. Please sign back in to continue.

References

Figures

Grahic Jump Location
Boundary layer bleed system of the NASA transonic flutter cascade facility
Grahic Jump Location
View of cascade test section
Grahic Jump Location
Effect of incidence angle on pressure coefficient compute with RVCQ3D
Grahic Jump Location
Cascade configuration C_20.0/30.0
Grahic Jump Location
Effects of sidewall boundary layer bleed rate
Grahic Jump Location
Effects of sidewall bleed on spanwise Mach number distribution at y/W=0.388 and x/C=−0.254
Grahic Jump Location
Effects of sidewall bleed on spanwise distribution of flow incidence angles at y/W=0.388 and x/C=−0.254
Grahic Jump Location
Effects of sidewall bleed on blade loading
Grahic Jump Location
Cascade flowfield for Mach number 1.35
Grahic Jump Location
Mach contours computed with PCSTAGE for original configuration C_20.0/30.0
Grahic Jump Location
Cascade turning angle versus inlet Mach number computed with RVCQ3D
Grahic Jump Location
Particle traces computed with RVCQ3D
Grahic Jump Location
Cascade configuration C_20.0/24.0
Grahic Jump Location
Mach contours computed with PCSTAGE for final configuration C_20.0/24.0
Grahic Jump Location
Wall static distributions for cascade configuration C_20.0/24.0
Grahic Jump Location
Blade loading diagrams for middle blade (B5) for cascade configuration C_20.0/24.0
Grahic Jump Location
Blade loading periodicity for configuration C_20.0/24.0

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