Unsteady aerodynamic analysis of supersonic through-flow fan with vibrating blades under non-zero mean loading

Toshiya Hanada, M. Namba

Research output: Contribution to journalArticle

2 Citations (Scopus)

Abstract

The double linearization concept is applied to a rotating annular cascade model operating at supersonic axial velocity. It is assumed that each blade vibrates with infinitesimal displacement amplitude under small but non-zero mean loading. Vibration modes normal and parallel to the blade chord are considered. Numerical results indicate that the mean loading effects play a crucial role on the aerodynamic instability of the blade motion. The bending motion can be unstable due to the presence of mean loading. Both the steady performance and the flutter boundary are highly sensitive to the blade camber. The bending motion instability is substantially influenced also by the chordwise component of the blade motion. Some numerical results compared with strip theory predictions demonstrate significant three-dimensional effects on the unsteady aerodynamic force under non-zero mean loading.

Original languageEnglish
Pages (from-to)709-750
Number of pages42
JournalJournal of Sound and Vibration
Volume194
Issue number5
DOIs
Publication statusPublished - Aug 1 1996

Fingerprint

unsteady aerodynamics
supersonic flow
blades
fans
Fans
Aerodynamics
Signal filtering and prediction
Cambers
Flutter (aerodynamics)
Linearization
camber
aerodynamic forces
flutter
linearization
aerodynamics
vibration mode
strip
cascades
predictions

All Science Journal Classification (ASJC) codes

  • Condensed Matter Physics
  • Mechanics of Materials
  • Acoustics and Ultrasonics
  • Mechanical Engineering

Cite this

Unsteady aerodynamic analysis of supersonic through-flow fan with vibrating blades under non-zero mean loading. / Hanada, Toshiya; Namba, M.

In: Journal of Sound and Vibration, Vol. 194, No. 5, 01.08.1996, p. 709-750.

Research output: Contribution to journalArticle

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