Numerical Modeling of Internal Flow Aerodynamics. Part 1: Steady State Computations

Abstract

Internal ballistics in a SRM can be solved with various ways and for various objectives 2. The motor design engineer wants to predict or understand the burning characteristics and the global performances of the motor, seek the efficiency of thermal insulation and nozzle design, check the reliability of ignition and motor design for the life cycle of the motor, take into account variability induced by manufacturing processes, etc.

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Document Details

Document Type
Technical Report
Publication Date
Jan 01, 2004
Accession Number
ADA425844

Entities

People

  • Jean-francois Guery

Tags

Communities of Interest

  • Energy and Power Technologies
  • Weapons Technologies

DTIC Thesaurus Topics

  • Boundary Layer
  • Burning Rate
  • Chemical Reactions
  • Combustion
  • Computational Fluid Dynamics
  • Computations
  • Fluid Dynamics
  • Fluid Flow
  • Heat Transfer
  • Mechanical Properties
  • Mechanics
  • Rocket Engines
  • Solid Propellants
  • Specific Heat
  • Steady State
  • Three Dimensional
  • Viscous Flow

Fields of Study

  • Engineering

Readers

  • Computational Fluid Dynamics (CFD)
  • Rocket Propulsion.
  • Software Engineering

Technology Areas

  • Microelectronics
  • Microelectronics - Microelectromechanical Systems