Pressure Based High Order TVD Methodology for Dynamic Stall Control.

Abstract

The objectives were to study various dynamic stall control concepts using a code developed under Phase I. The concepts studied were; vortex flaps, apex fence flaps, forebody strakes, spanwise blowing, leading edge blowing and suction, and forebody blowing and suction.

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Document Details

Document Type
Technical Report
Publication Date
Nov 01, 1994
Accession Number
ADA290149

Entities

People

  • A. J. Przekwas
  • H. Q. Yang
  • V. J. Harrand
  • Z. J. Wang

Tags

Communities of Interest

  • Air Platforms
  • Space
  • Weapons Technologies

DTIC Thesaurus Topics

  • Aerodynamic Characteristics
  • Aerodynamic Configurations
  • Air Force
  • Aircrafts
  • Boundary Layer
  • Computational Fluid Dynamics
  • Control Surfaces
  • Delta Wings
  • Flow Visualization
  • Fluid Dynamics
  • Fluid Flow
  • Leading Edges
  • Mechanical Phenomena
  • Physics Laboratories
  • Three Dimensional
  • Two Dimensional

Fields of Study

  • Physics

Readers

  • Aerodynamics/Aeronautics.
  • Computational Fluid Dynamics (CFD)