Investigation of Magnetohydrodynamic (MHD) Controlled Inlet with Nonequilibrium MHD Generator

Abstract

This report results from a contract tasking Leninetz Holding Company, NIPGS as follows: The contractor will analytically investigate applying magneto hydrodynamic (MHD) generators to a generic hypersonic inlet. The inlet geometry will be a two-shock inlet with the total turning angle of 15 and designed for Mach 10. The contractor will evaluate the location and configuration of electromagnet coils and electrodes for the MHD system. Flow fields in the MHD controlled inlet will be calculated in 2D Euler approach. Analysis of elementary processes responsible for flow ionization will be assessed. Space distribution for power density deposited in the flow and for conductivity of flow due to e-beam propagation will be calculated, A mathematical model of the MHD-controlled inlet with non-equilibrium MHD generators using e-beams as the ionizer will be developed. Finally, flow fields in the MHD-controlled inlet will be calculated in a wide range of parameters (altitude, Mach number contraction ratio, MHD and ionizer parameters. The main characteristics of the inlet will be determined such as the air mass flow-rate flow compression and total pressure recovery. Requirements for the magnetic system and ionizer, which ensure efficient control of inlet at off-design conditions, will be formulated.

Open PDF

Document Details

Document Type
Technical Report
Publication Date
Dec 01, 2006
Accession Number
ADA465270

Entities

People

  • Alexander L. Kuranov

Tags

Communities of Interest

  • Energy and Power Technologies

DTIC Thesaurus Topics

  • Air Force
  • Air Masses
  • Charged Particles
  • Computational Fluid Dynamics
  • Elastic Scattering
  • Electron Energy
  • Electrons
  • Flow Fields
  • Flow Rate
  • Fluid Dynamics
  • Generators
  • Geometry
  • Mach Number
  • Mass Flow
  • Mathematical Models
  • Monte Carlo Method
  • Two Dimensional

Fields of Study

  • Physics

Readers

  • Aerodynamics.
  • Electrical Engineering
  • Pulsed Power and Plasma Physics.

Technology Areas

  • Hypersonics
  • Hypersonics - Hypersonic Flight
  • Hypersonics - Hypersonic Flow
  • Space
  • Space - Hall-Effect Thruster