HOT CYCLE ROTOR SYSTEM THERMAL ANALYSIS, PART II

Abstract

A survey is given of estimated temperatures in the blade root and hub section of the initial hot cycle rotor. Initial thermal analysis indicated a necessity of applying insulation to prevent high temperatures in this area. Aluminum clad shields were subsequently installed over the hot gas ducting. Due to the conservative approach used in the calculations, the highest predicted component temperatures remain much below acceptable limits. No thermal problems are anticipated in this area of the rotor.

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Document Details

Document Type
Technical Report
Publication Date
Mar 01, 1962
Accession Number
AD0288502

Entities

People

  • J. W. Rabek

Tags

Communities of Interest

  • Air Platforms

DTIC Thesaurus Topics

  • Air Flow
  • Air Gaps
  • Aircrafts
  • Airframes
  • Aluminum
  • Exhaust Gases
  • Flow
  • Gases
  • Government Procurement
  • Heat Energy
  • Heat Transfer
  • Heat Transfer Coefficients
  • Heat Transmission
  • High Temperature
  • Hot Gases
  • Thermal Analysis
  • Turbojet Engines

Readers

  • Aerodynamics.
  • Systems Analysis and Design
  • Thermal Physics or Thermal Science.

Technology Areas

  • Microelectronics
  • Microelectronics - Microelectromechanical Systems