Hypersonic Flows Over Conical Bodies with Asymmetric Bluntness

Abstract

The authors have also elaborated a program system for calculation of flows around such kind of body which includes programs for calculation of sub and supersonic flow regions using methods of transition to a steady state and calculation of X-hyperbolic flow region using different modifications of the Godunov method. Viscous effects in this program system are taken into account basing on auxiliary approach of the theory of boundary layer.

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Document Details

Document Type
Technical Report
Publication Date
Jul 01, 2002
Accession Number
ADA409064

Entities

People

  • N. S. Bachmanova
  • V. A. Kozlovskii
  • V. N. Andreev
  • V. V. Eremin
  • Yu. M. Lipnitskii

Tags

DTIC Thesaurus Topics

  • Aerodynamic Characteristics
  • Applied Mechanics
  • Asymmetry
  • Bodies
  • Boundary Layer
  • Coefficients
  • Conical Bodies
  • Experimental Data
  • Flow
  • Fluid Dynamics
  • Hypersonic Flow
  • Hypersonic Wind Tunnels
  • Mach Number
  • Shape
  • Spacecraft
  • Vehicles
  • Wind Tunnels

Fields of Study

  • Physics

Readers

  • Finite Element Method (FEM) for solving Partial Differential Equations (PDEs)
  • Fluid Mechanics and Fluid Dynamics.
  • Systems Analysis and Design

Technology Areas

  • Hypersonics
  • Hypersonics - Hypersonic Boundary Layers
  • Hypersonics - Hypersonic Flight