Flow Characteristics in Solid Fuel Ramjets.

Abstract

An experimental investigation of the internal ballistics of solid fuel ramjets was conducted in order to determine the effects of inlet step size, inlet velocity and wall blowing on flow characteristics behind a backward facing step inlet. It was shown that the reattachment point (zone) moves toward the step inlet with wall mass addition at a constant inlet mass flux. For a given step inlet, however, the leading edge of the reattachment zone was stationary with variations in inlet velocity. A point where the wall temperature and centerline static pressure profiles leveled off simultaneously was defined as the end of the reattachment zone. This zone spread out (grew thicker) both with increasing inlet velocity for a given step size, and with increasing step height. Maximum wall temperatures occurred downstream of the reattachment zone. (Author)

Document Details

Document Type
Technical Report
Publication Date
Jul 01, 1974
Accession Number
AD0786692

Entities

People

  • David W. Netzer
  • Joseph T. Phaneuf Jr.

Organizations

  • Naval Postgraduate School

Tags

DTIC Thesaurus Topics

  • Ballistics
  • Dynamic Pressure
  • Fuels
  • Leading Edges
  • Solid Fuels
  • Static Pressure
  • Stationary

Fields of Study

  • Physics

Readers

  • Combustion and Flow Dynamics.
  • Fluid Mechanics and Fluid Dynamics.