Status of Advanced Boundary Layer Code Development for SRM Nozzle Ablation Including Two Phase Flow Effects

Abstract

Briefing charts overview of the Integrated High Payoff Rocket Propulsion Technology(IHPRPT) Phase III Solid Rocket Motor Modeling Program.

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Document Details

Document Type
Technical Report
Publication Date
Aug 01, 2004
Accession Number
ADA427803

Entities

People

  • Al Murray
  • Brian Mclaughlin
  • Derek Gonzalez
  • Kent Hennessey
  • Mark Eagar

Organizations

  • Aerojet Rocketdyne Holdings

Tags

DTIC Thesaurus Topics

  • Ablation
  • Blast Tubes
  • Boundaries
  • Boundary Layer
  • Chambers
  • Combustion
  • Computational Fluid Dynamics
  • Equations Of State
  • Flow
  • Flow Fields
  • Geometry
  • Layers
  • Materials
  • Particles
  • Phase
  • Two Dimensional
  • Two Phase Flow

Fields of Study

  • Physics

Readers

  • Defense Acquisition Program Management
  • Fluid Dynamics.
  • Rocket Propulsion.