TRANSONIC ROTATIONAL FLOW OVER A CONVEX CORNER

Abstract

A singularity is encountered in the flow field about two-dimensional and axisymmetric bodies characterized by a sharp corner, where the fluid velocity becomes sonic. An investigation of this sonic singularity, and the application of results to the analysis of flow fields about blunt bodies are presented. It is shown that the problem belongs to the family of asymptotic or boundary layer phenomena of mathematical physics. The solution of the first approximation equations is given by a series in powers of a variable measuring the distance from the corner with coefficients depending on an appropriate similarity variable. The leading coefficient of the series is independent of three-dimensional and rotationality effects, in complete analogy to the well-known solution of the corner problem in supersonic flow. Results are presented for the leading singularity and for the first two corrections due to rotationality and axial symmetry of the flow. (Author)

Document Details

Document Type
Technical Report
Publication Date
Aug 01, 1959
Accession Number
AD0264409

Entities

People

  • Roberto Vaglio-laurin

Organizations

  • New York University Tandon School of Engineering

Tags

DTIC Thesaurus Topics

  • Axisymmetric
  • Blunt Bodies
  • Bodies
  • Boundary Layer
  • Coefficients
  • Flow
  • Flow Fields
  • Supersonic Flow
  • Symmetry
  • Three Dimensional
  • Two Dimensional

Fields of Study

  • Physics

Readers

  • Fluid Dynamics.
  • Theoretical Analysis.

Technology Areas

  • Hypersonics
  • Hypersonics - Hypersonic Flight