Quiet Shrouded Circulation Control Propeller.

Abstract

The patent application describes a propeller capable of generating high thrust at reduced noise levels, weight and drag. The propeller blades employ a tangential slot along the trailing edge of each propeller blade and circulation control blowing from the tangential slot over the trailing edge. Lift is generated by the coanda blowing. The lift is proportional to the momentum flow of the air out of the slot and is substantially independent of the rotational velocity. Additionally a circulation control shroud expands the thrusting slipstream of the propeller so that the shroud diffusion angle is increased and the average exit velocity is reduced, thereby increasing efficiency and reducing noise.

Document Details

Document Type
Technical Report
Publication Date
Jul 11, 1974
Accession Number
ADD001177

Entities

People

  • Robert M. Williams

Organizations

  • United States Department of the Navy

Tags

DTIC Thesaurus Topics

  • Blades
  • Diffusion
  • Efficiency
  • Momentum
  • Patent Applications
  • Patents
  • Propeller Blades
  • Propellers
  • Slipstream
  • Trailing Edges

Fields of Study

  • Physics

Readers

  • Combustion and Flow Dynamics.
  • Fluid Mechanics and Fluid Dynamics.
  • Marine Hydrodynamics