HOT FIRING EVALUATION OF SPIRAL WOUND RIBBON STRUCTURES FOR TRANSPIRATION/FILM COOLING.

Abstract

The work reported in this Third Quarterly Report consisted of continuation of the fabrication of the test engine components and the initiation of the test operations. Fabrication of the test engine components were completed except for the spiral wound ribbon test items which have been delayed by materials and fabrication problems. Test operations with the uncooled hardware has commenced and injector performance has been documented over the range of test conditions.

Document Details

Document Type
Technical Report
Publication Date
Jan 01, 1967
Accession Number
AD0805991

Entities

People

  • A. Robert Nagy Jr.
  • Hirosh Shimizu
  • John E. Ahern

Tags

DTIC Thesaurus Topics

  • Cooling
  • Engine Components
  • Engines
  • Fabrication
  • Film Cooling
  • Injectors
  • Materials

Fields of Study

  • Physics

Readers

  • Aerospace Test and Evaluation
  • Combustion and Flow Dynamics.
  • Technical Research and Report Writing.