ON GENERALIZED SOLUTIONS TO THE INVISCID THREE-DIMENSIONAL PERTURBATION EQUATIONS IN A HYPERBOLIC REGION. VOLUME I. THEORETICAL RESULTS

Abstract

A method of determining generalized solutions to the three-dimensional small perturbation equations for supersonic flow is derived. By means of integral and matrix transformations, series solutions for the perturbation quantities u, v, w, p, and rho are obtainable at the intersection point of characteristics in a transformed plane. (Author)

Document Details

Document Type
Technical Report
Publication Date
Sep 14, 1962
Accession Number
AD0288676

Entities

People

  • C.r. Ortloff

Organizations

  • The Aerospace Corporation

Tags

Communities of Interest

  • Air Platforms

DTIC Thesaurus Topics

  • Equations
  • Flow
  • Integrals
  • Mathematics
  • Perturbations
  • Supersonic Flow
  • Three Dimensional

Fields of Study

  • Mathematics
  • Physics

Readers

  • Fluid Dynamics.

Technology Areas

  • Hypersonics
  • Hypersonics - Hypersonic Boundary Layers