STUDY OF HYPERSONIC CONTAMINATED WAKE BY AN EXACT NUMERICAL SOLUTION,

Abstract

A theoretical study is presented of hypersonic wake with and without contaminants. The nonlinear coupling equations of gas dynamics and chemical kinetics are solved numerically by a finite-difference scheme. Typical calculations of laminar and turbulent non-equilibrium wake are shown for a slender body with square root of (C sub D) (A) approximately equal to 10 cm. The results indicate that the air system and the air-plus-sodium system are in non-equilibrium at the altitude of 100,000 ft. This non-equilibrium characteristic may exist at even lower altitudes. The effects of sodium on the electron concentration are important. Since the deionization processes of sodium are relatively slow, the sodium-contaminated wake has a longer electron trail. (Author)

Document Details

Document Type
Technical Report
Publication Date
Dec 01, 1963
Accession Number
AD0429309

Entities

People

  • Huon Li

Organizations

  • General Electric

Tags

DTIC Thesaurus Topics

  • Altitude
  • Bodies
  • Chemical Kinetics
  • Contracts
  • Couplings
  • Deionization
  • Dynamics
  • Electrons
  • Environmental Pollutants
  • Equations
  • Gas Dynamics
  • Kinetics
  • Mathematics
  • Slender Bodies
  • Square Roots

Fields of Study

  • Physics

Readers

  • Finite Element Method (FEM) for solving Partial Differential Equations (PDEs)
  • Fluid Dynamics.
  • Molecular Photonics/Laser Physics

Technology Areas

  • Hypersonics
  • Hypersonics - Hypersonic Flight
  • Microelectronics