STORAGE HEATER DESIGN STUDY FOR THE HYPERSONIC TRUE TEMPERATURE TUNNEL

Abstract

The results of a design study of a ceramic storage heater system for the Tripltee wind tunnel are presented. The heater is designed to supply 1500 lb/sec of air at 2000 psi and 3900 R for a period of 30 sec. Emphasis was placed on the application of improved refractory materials and shapes for the heat storage matrix to achieve a large reduction in total heater size and dust carry-over. Heating of the storage matrix with combustion products and the flow processes involved pressurizing the heater were analyzed. A heater design concept is presented and the advantages accruing from use of matrix elements specifically designed for this application are indicated. Procedures for procuring refractory elements having the requisite properties are outlined. A second Tripltee design requirement is for 5000 lb/sec of air at 400 psi and 1600 R for 30 sec. The problem of achieving this flow condition by mixing hot air from the heater with cold air was studied and a design concept for a mixer developed.

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Document Details

Document Type
Technical Report
Publication Date
Jul 01, 1964
Accession Number
AD0442305

Entities

People

  • B. C. Lindahl
  • D. G. Decoursin
  • F. W. Larsen
  • W. S. Hedrick

Tags

Communities of Interest

  • Ground and Sea Platforms

DTIC Thesaurus Topics

  • Air Force
  • Bricks
  • Construction
  • Creep
  • Crystal Structure
  • Heat Transfer
  • Heat Transmission
  • Manufacturing
  • Materials
  • Mechanical Properties
  • Mechanical Working
  • Mechanics
  • Modulus Of Elasticity
  • Refractory Materials
  • Test And Evaluation
  • Test Facilities
  • Thermal Conductivity

Fields of Study

  • Physics

Readers

  • Fluid Dynamics.
  • Systems Analysis and Design
  • Thermal Physics or Thermal Science.

Technology Areas

  • Hypersonics
  • Hypersonics - Hypersonic Flow