Study of the Boundary Layer in the Inboard Sections of a Tilt-Rotor Blade by Embedded LDV Measurements

Abstract

This report focuses on the boundary layer (BL) velocity distribution in the inboard region of a tiltrotor blade. The instrumentation consists of a Laser Doppler Velocimeter embedded in the inboard region of the blade. This set up allows measuring the chordwise and spanwise component of the boundary layer velocity from a distance of 0.3 mm to 20 mm along a direction normal to the blade surface. The experiments were carried out on a two-bladed rotor with a blade geometry close to the one of CAMRAD II model of TRAM. The blade section located at r/R=0.3 was explored in three abscissa x/C=0.10; 0.33; 0.54, and for 3 pitch angles, two of them at values lower than the static stall angle of incidence, the third at a higher value. During the tests the tip Mach number was maintained constant at M(sub tip)=0.22. Results obtained on the velocity components have allowed characterizing the different aspects of the BL. At low incidences, chordwise velocity profiles exhibit a turbulent behavior (power law in 1/n) for x/C=0.33 and 0.54. At the chord station x/C=0.10, the BL is very thin with a laminar velocity profile. At the incidence higher than the static stall one, it is worthy to note that the chordwise velocity profile at x/C=0.3 shows an attached turbulent BL, while at x/C=0.54 the velocity profile begins to deviate from a turbulent shape to a separated one that produces the thickening of the BL and an evolution of the profile to a velocity distribution with an inflexion point. This result confirms the delay of the BL separation due to rotation, already observed. At the leading edge (x/C=0.1), and for the present low rotational speed OMEGA, the velocity distribution in the BL seems to point out a transitional zone inside of which the randomness of the velocity intensity attests to a high vorticity that may be due to a leading edge vortex or a bubble formation sustaining during the rotation the reattachment of the BL as observed at x/C=0.33.

Open PDF

Document Details

Document Type
Technical Report
Publication Date
Jul 01, 2003
Accession Number
ADA420100

Entities

People

  • Charlie Barla
  • Christian Maresca
  • Daniel Favier
  • Eric Berton
  • Marcellin Nsi Mba

Tags

Communities of Interest

  • Air Platforms

DTIC Thesaurus Topics

  • Aerodynamic Characteristics
  • Aircrafts
  • Airframes
  • Angle Of Incidence
  • Boundary Layer
  • Computational Fluid Dynamics
  • Flow
  • Fluid Mechanics
  • Geometry
  • Layers
  • Leading Edges
  • Mach Number
  • Measurement
  • Mechanical Properties
  • Three Dimensional
  • Tilt Rotor Aircraft
  • Velocimeters

Fields of Study

  • Physics

Readers

  • Aerodynamics.
  • Astronomy/Astrophysics
  • Fluid Dynamics.

Technology Areas

  • Directed Energy