Optimum fan pressure ratio for bypass engines with separate or mixed exhaust streams
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[1] Jack D. Mattingly,et al. Elements of Gas Turbine Propulsion , 1996 .
[2] J. F. V. Vincent,et al. Deployable Structures in Nature: Potential for Biomimicking , 2000 .
[3] Henry Cohen,et al. Gas turbine theory , 1973 .
[4] G L Wilde. FUTURE LARGE CIVIL TURBOFANS AND POWERPLANTS , 1978 .
[5] Marcelo Alonso,et al. Mechanics and thermodynamics , 1980 .
[6] P. C. Ruffles. The future of aircraft propulsion , 2000 .
[7] A. Guha. An efficient generic method for calculating the properties of combustion products , 2001 .
[8] Abhijit Guha. Optimisation of aero gas turbine engines , 2001 .
[9] N. T. Birch. 2020 vision : the prospects for large civil aircraft propulsion , 2000 .
[10] Paul I. King,et al. Identifying Optimal Fan Compressor Pressure Ratios for the Mixed-Stream Turbofan Engine , 2000 .
[11] A. J. B. Jackson. Some Future Trends in Aero Engine Design for Subsonic Transport Aircraft , 1976 .