Wind Tunnel Analysis of Helicopter Aerodynamics with Varying Rotor Head Blade Stub Lengths

Ulrich Hartmann, Johannes Ruhland, Christian Breitsamter

Research output: Chapter in Book/Report/Conference proceedingChapterpeer-review

Abstract

Experimental investigations are performed on a helicopter wind tunnel model for three rotor heads with different blade stub lengths. This investigation is intended to judge the influence of the blade stub spanwise dimension on the drag, lift, and especially pitching moment characteristics. Aerodynamic forces, moments, and the wake flow fields are analyzed. As expected, the longest blade stubs provide the highest drag and lift coefficient along the angle of attack polar, while both shorter blade stubs show a similar force course. The flow field of the largest rotor head exhibits pronounced blade tip vortices, which influence the pitching moment polar at high angles of attack. The medium and long stubs show a similar flow field, while the hubcap vortex dominates the smallest blade stub configuration.

Original languageEnglish
Title of host publicationNotes on Numerical Fluid Mechanics and Multidisciplinary Design
PublisherSpringer Science and Business Media Deutschland GmbH
Pages613-622
Number of pages10
DOIs
StatePublished - 2024

Publication series

NameNotes on Numerical Fluid Mechanics and Multidisciplinary Design
Volume154
ISSN (Print)1612-2909
ISSN (Electronic)1860-0824

Keywords

  • blade stubs
  • helicopter
  • rotor wake

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