In this solution some basic concepts and formulas of Turbo-Machinery are used. For more information, refer to any standard textbook or drop a comment below. Please give a Thumbs Up, if solution is helpful.
Solution :
NOTE : Feel free to ask
further queries. Your positive rating would be appreciated and
motivate me !
Use the following test results to estimate the overall isentropic efficiency of a single-sided ce...
A single-spool turbofan engine has the following data Ambient temperature Ambient pressure BPR Overall pressure ratio Fan pressure ratio Fuel heating value Turbine inlet temperature Diffuser pressure recovery factor Compressor efficiency Fan efficiency Combustion efficien Burner pressure recovery factor Turbine efficiency Nozzle efficiency Flight Mach number 288 K 101.3 kN/m2 0.7 25 3.375 44,000 kJ/kg 2000 K 0.9 0.89 0.91 0.98 0.95 0.98 1.0 0.3 Calculate 1. 2. 3. Thrust per unit mass flow rate TSFC Thermal, propulsive and overall...
Just use results from Test No. 1 and other info provided.
Air box orifice =15mm Atmospheric pressure, Pu = 101.3 kPa Inclined manometer slope = 1:5 Air box diameter = 300mm Item: Test No. 1: Test No. 2: Motor speed 1, rpm, N1 1 300 1 400 Compressor speed 1, 651 704 rpm, NZ 830 900 19.4°C 19.5°C Power inputs, watts Ambient temperature, T1 Stage 1 compressor outlet, T2 90.8°C 74.5°C 17°C 17.4°C Water inlet, Tw1 Water outlet, Tw2 18.1°C...
Use a simple Brayton cycle gas turbine as the baseline for the
following questions. Use a cold-air-standard analysis (R=0.287
kJ/kg-K, k=Cp/Cv=1.40, Cp= (k/(k-1))*R = 1.0045 kJ/kg-K) with the
following specifications:
Use a simple Brayton cycle gas turbine as the baseline for the following questions. Use a cold-air-standard analysis (R=0.287 kJ/kg-K, k=Cp/Cv=1.40, Cpr (k/(k-1))*R = 1.0045 kJ/kg-K) with the following specifications: Mass Inlet Press. Pressure Turbine Isentropic Eff Neglect combustion chemistry Flowrate T p Ratio Inlet T Comp Turb Neglect minor...