Finite Difference Calculation of an Inviscid Transonic Flow over Oscillating Airfoils,

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Document Details

Document Type
Technical Report
Publication Date
Oct 01, 1980
Accession Number
ADA123982

Entities

People

  • T. Ishiguro

Organizations

  • Royal Aircraft Establishment

Tags

Communities of Interest

  • Air Platforms
  • Energy and Power Technologies

DTIC Thesaurus Topics

  • Air Force
  • Boundary Layer
  • Contours
  • Coordinate Systems
  • Differential Equations
  • Equations
  • Euler Equations
  • Flow Fields
  • Fluid Dynamics
  • Free Stream
  • Frequency
  • Inviscid Flow
  • Mach Number
  • Pressure Distribution
  • Steady Flow
  • Two Dimensional
  • Unsteady Flow