THEORETICAL ANALYSIS OF THE FLOW AND DRAG OF SURFACE IRREGULARITIES IMMERSED IN A WALL-LAYER STREAM IN A SUPERSONIC MAIN STREAM

Abstract

A two-dimensional inviscid compressible flow over an arbitrarily shaped surface irregularity immersed in single or double wall-layer streams parallel to a supersonic main stream is analyzed. Solutions for single-layer streams are obtained on a linearized two-dimensional basis for the complete flow field. Solutions for double-layer streams are obtained on a linearized quasi onedimensional basis for the layer streams and on a linearized two-dimensional basis for the main stream. The double-layer stream is considered as an idealization of a boundary layer, and has possible application to the determination of the influence of a boundary layer on the wave drag of a surface irregularity submerged in the boundary layer. Comparison of pressure distributions and wave-drag calculations by the quasi one-dimensional method with limited experiments is not completely satisfactory for dominantly subsonic layer streams, but holds promise for turbulent boundary layers for Mach numbers around 2.0 and higher. (Author)

Document Details

Document Type
Technical Report
Publication Date
Oct 01, 1961
Accession Number
AD0271376

Entities

People

  • Henry W. Woolard

Organizations

  • Johns Hopkins University Applied Physics Laboratory

Tags

DTIC Thesaurus Topics

  • Boundaries
  • Boundary Layer
  • Compressible Flow
  • Flow
  • Flow Fields
  • Layers
  • Pressure Distribution
  • Turbulent Boundary Layer
  • Two Dimensional

Fields of Study

  • Physics

Readers

  • Calculus or Mathematical Analysis
  • Fluid Mechanics and Fluid Dynamics.
  • Structural Dynamics.

Technology Areas

  • Hypersonics
  • Hypersonics - Hypersonic Boundary Layers