Rotor/Body Aerodynamic Interactions

Abstract

A wind-tunnel investigation was conducted in which independent, steady-state aerodynamic forces and moments were measured on a 2.24-m-diam, two- bladed helicopter rotor and on several different bodies. The objective was to determine the mutual interaction effects for variations in velocity, thrust, tip-path-plane angle of attack, body angle of attack, rotor/body position, and body geometry. the results of the investigation show that the body longitudinal aerodynamic characteristics are significantly affected by the presence of a rotor and hub, and that the hub interference may be a major part of such interaction. This report presents the effects of various parameters on the interactions and discusses the difficulties encountered in determining the effect of the body on the rotor performance.

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Document Details

Document Type
Technical Report
Publication Date
Oct 01, 1983
Accession Number
ADA135040

Entities

People

  • Charles A. Smith
  • Mark D. Betzina
  • Patrick Shinoda

Organizations

  • National Aeronautics and Space Administration

Tags

DTIC Thesaurus Topics

  • Aerodynamic Characteristics
  • Aerodynamic Configurations
  • Army Aviation
  • Drive Shafts
  • Dynamic Pressure
  • Free Stream
  • Geometry
  • Helicopter Rotors
  • Helicopters
  • Measurement
  • Pressure Distribution
  • Pressure Measurement
  • Standards
  • Static Pressure
  • Tail Rotors
  • United States
  • Wind Tunnels

Fields of Study

  • Physics

Readers

  • Aerodynamics.
  • Aerodynamics/Aeronautics.