Wake dynamics and rotor-fuselage aerodynamic interactions

A.R. Kenyon, R.E. Brown

Research output: Contribution to journalArticlepeer-review

43 Citations (Scopus)
146 Downloads (Pure)


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.
Original languageEnglish
Pages (from-to)12003-1-12003-18
Number of pages18
JournalJournal of the American Helicopter Society
Issue number1
Publication statusPublished - 1 Jan 2009


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

Cite this