Tables of the Thermodynamic Properties of Air and the Exhaust Gas from a Turbine Engine

Abstract

Thermodynamic properties of air and the exhaust gas from a turbine engine (C(n)H(1.95n))/Air System) are presented in tabular form. The properties presented air enthalpy (h), entropy (s), and specific heat at constant pressure (cp). The properties of air are presented for a temperature range from 300 to 1, 800R and a pressure range from 0.5 to 600 psia. The properties of exhaust gas are presented for a temperature range from 600 to 4,000R, a pressure range from 0.5 to 600 psia, and a fuel-to-air ratio from 0.005 to 0.067.

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Document Details

Document Type
Technical Report
Publication Date
Mar 01, 1976
Accession Number
ADA021954

Entities

People

  • John M. Pelton
  • K. L. Hannah

Organizations

  • Arnold Engineering Development Complex

Tags

DTIC Thesaurus Topics

  • Air Force
  • Enthalpy
  • Exhaust Gases
  • Gases
  • Government Procurement
  • Governments
  • Specific Heat
  • Tennessee
  • Test Facilities
  • Thermodynamic Properties
  • Three Dimensional
  • Turbines
  • United States

Readers

  • Combustion and Flow Dynamics.
  • Polymer Science and Technology