Theoretical Aerodynamics.

Abstract

Mathematical and computational studies have been carried out on problems on theoretical aerodynamics. Shock free bodies and optimum critical airfoils have been considered in transonic theory, optimum three-dimensional lifting wings in hypersonic theory. Stability and transition of boundary layers has been analyzed according to triple deck theory. The Benjamin-Davis-Acrivos equation has been derived and it has been shown how solitons can lead to chaotic motion.

Open PDF

Document Details

Document Type
Technical Report
Publication Date
Jan 10, 1996
Accession Number
ADA310010

Entities

People

  • Julian D. Cole

Organizations

  • Air Force Office of Scientific Research

Tags

Communities of Interest

  • Air Platforms
  • Human Systems

DTIC Thesaurus Topics

  • Aerodynamics
  • Applied Mathematics
  • Bodies
  • Boundary Layer
  • Computational Fluid Dynamics
  • Computational Science
  • Equations
  • Euler Equations
  • Flow
  • Fluid Dynamics
  • Fluid Flow
  • Layers
  • Mach Number
  • Mathematics
  • Shock Waves
  • Sonic Boom
  • Three Dimensional

Fields of Study

  • Physics

Readers

  • Aerodynamics/Aeronautics.
  • Fluid Dynamics.

Technology Areas

  • Hypersonics
  • Hypersonics - Hypersonic Boundary Layers