Sunday, October 14, 2018

GAS TURBINE THERMODYNAMIC AND PERFORMANCE ANALYSIS METHODS USING AVAILABLE CATALOG DATA



Content :-
  • Typical open gas turbine 
  • T-S diagram for closed gas turbine cycle 
  • Ambient Temperature Power Correction Factor Curve.
  • Effect of ambient temperature and air to fuel ratio on thermal efficiency.
  • Representative Altitude Power Correction Factor Curve. 
  • Open gas turbine and T-S diagram.
  • Relation between pressure ratio and efficiency.
  • Variation of compression ratio and turbine inlet temperature on thermal efficiency.
  • Variation of compression ratio and ambient temperature on thermal efficiency.
  • Variation of turbine inlet temperatures with thermal efficiency for several compression ratio and air to fuel ratio. 
  • Effect of isentropic compressor efficiency air to fuel ratio on thermal efficiency.
  • Effect of isentropic turbine efficiency air to fuel ratio on thermal efficiency.
  • T-S diagram for compression and expansion.
  • T-S diagram for compression process.
  • Pressure losses and pressure ratios in the compressor.
  • GUI of the EES model.
  • The pressure values in the compressor.
  • The pressure values in the turbine .
  • Difference between the Cp (Mathcad) and Cp(EES) for dry air (200K-2150K).
  • Difference between the Cp (Mathcad) and Cp(EES) for Methane (200K-2250K)
  • Difference between the Cp(Mathcad) and Cp(EES) for water (200K-2250K).
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