Identifying Optimal Fan Compressor Pressure Ratios for the Mixed-Stream Turbofan Engine-Reference-Cited by-同舟云学术

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Identifying Optimal Fan Compressor Pressure Ratios for the Mixed-Stream Turbofan Engine

Published:2000-01 Issue:1 Volume:16 Page:79-86
ISSN:0748-4658
Container-title:Journal of Propulsion and Power
language:en
Short-container-title:Journal of Propulsion and Power

Author:

Millhouse Paul T.¹,Kramer Stuart C.²,King Paul I.²,Mykytka Edward F.³

Affiliation:

1. NRO, Chantilly,Virginia, 20151-1715

2. Air Force Institute of Technology, Wright–Patterson Air Force Base, Ohio 45433-7765

3. University of Dayton, Dayton, Ohio 45469

Publisher

American Institute of Aeronautics and Astronautics (AIAA)

Subject

Space and Planetary Science,Mechanical Engineering,Fuel Technology,Aerospace Engineering

Link

http://arc.aiaa.org/doi/pdf/10.2514/2.5534

Reference6 articles.

1. 1Mattingly, J., Heiser, W., and Daley, D., Aircraft Engine Design, AIAA Education Series, AIAA, New York, 1987, pp.10-217.

2. Mattingly, J., Elements of Gas Turbine Propulsion, McGraw-Hill, New York, 1996, pp.551-560.

3. Arora, J., Introduction to Optimum Design, McGraw-Hill, New York, 1989, pp.574-577.

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