INVESTIGATION OF VITIATED INLET-AIR EFFECTS ON TURBOJET ENGINE PERFORMANCE

Abstract

Laboratory test were conducted to investigate the effects of vitiated inlet-air on turbojet engine performance. The test vehicle was a J60-P-6 turbojet engine which was operated at sea level hot day inlet conditions for simulated flight Mach numbers of 0.0, 0.5, and 0.85. Effects of vitiated inlet- air were evaluated at vitiation levels of 1.7, 2.3, 3.0, and 3.5 percent.

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Document Details

Document Type
Technical Report
Publication Date
Jul 01, 1968
Accession Number
AD0673985

Entities

People

  • Daniel R. Snyder

Tags

Communities of Interest

  • Air Platforms

DTIC Thesaurus Topics

  • Air Flow
  • Air Heaters
  • Air Temperature
  • Aircrafts
  • Calorific Value
  • Chemical Reactions
  • Combustion
  • Combustion Products
  • Engines
  • Flowmeters
  • Gas Turbines
  • Heat Exchangers
  • Instrumentation
  • Jet Engines
  • Test Facilities
  • Turbines
  • Turbojet Engines

Fields of Study

  • Physics

Readers

  • Combustion science or combustion engineering.
  • Petroleum Engineering