Wake dynamics and rotor-fuselage aerodynamic interactions

A.R. Kenyon, R.E. Brown

Research output: Contribution to journalArticle

38 Citations (Scopus)

Abstract

The unsteady loads experienced by a helicopter are known to be strongly influenced by aerodynamic interactions between the rotor and fuselage; these unsteady loads can lead to deficiencies in handling qualities and unacceptable vibratory characteristics of the rotorcraft. This work uses a vorticity-based computational model to study the governing processes that underpin this aerodynamic interaction and aims to provide greater understanding of the wake dynamics in the presence of a fuselage, as well as an appreciation of how the geometry of the wake affects the loading on the fuselage. The well-known experiments using NASA's ROBIN fuselage are used to assess the accuracy of the computations. Comparisons of calculations against results from smoke visualization experiments are used to demonstrate the ability of the model to reproduce accurately the geometry of the rotor wake, and comparisons with inflow data from the experiments show the method to capture well the velocity field near to the rotor. The fuselage model is able to predict accurately the unsteady fuselage loading that is induced by blade passage and also by the inviscid interaction between the main rotor wake and fuselage.
LanguageEnglish
Pages12003-1-12003-18
Number of pages18
JournalJournal of the American Helicopter Society
Volume54
Issue number1
DOIs
Publication statusPublished - 1 Jan 2009

Fingerprint

Fuselages
Aerodynamics
Rotors
Geometry
Experiments
Vorticity
Smoke
Helicopters
NASA
Visualization

Keywords

  • aerodynamic interactions
  • rotor and fuselage
  • unsteady loads
  • vibratory characteristics
  • vorticity-based computational model
  • aerodynamic interaction
  • rotor wake

Cite this

Kenyon, A.R. ; Brown, R.E. / Wake dynamics and rotor-fuselage aerodynamic interactions. In: Journal of the American Helicopter Society. 2009 ; Vol. 54, No. 1. pp. 12003-1-12003-18.
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Wake dynamics and rotor-fuselage aerodynamic interactions. / Kenyon, A.R.; Brown, R.E.

In: Journal of the American Helicopter Society, Vol. 54, No. 1, 01.01.2009, p. 12003-1-12003-18.

Research output: Contribution to journalArticle

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