Aero Gas Turbine Flight Performance Estimation Using Engine Gas Path Measurements-Reference-Cited by-同舟云学术

Aero Gas Turbine Flight Performance Estimation Using Engine Gas Path Measurements

Published:2015-05 Issue:3 Volume:31 Page:851-860
ISSN:0748-4658
Container-title:Journal of Propulsion and Power
language:en
Short-container-title:Journal of Propulsion and Power

Author:

Li Yi-Guang¹

Affiliation:

1. School of Aerospace, Cranfield University, Cranfield, England MK43 0AL, United Kingdom

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/10.2514/1.B35381

Reference15 articles.

1. KoenigR. W.FishbachL. W. “GENENG—A Program for Calculating Design and off Design Performance for Turbojet and Turbofan Engines,” NASA TND-6552, 1972.

2. FishbachL. W.KoenigR. W. “GENENG II—A Program for Calculating Design and off Design Performance of Two and Three-Spool Turbofans With as Many Nozzles,” NASA TN-D-6553, 1972.

3. MacMillanW. “Development of a Modular Type Computer Program for the Calculation of Gas Turbine off Design Performance,” Ph.D. Thesis, Cranfield Inst. of Technology, Cranfield, England, U.K. 1974.

4. Adaptive Simulation of Gas Turbine Performance

5. Optimal Measurement and Health Index Selection for Gas Turbine Performance Status and Fault Diagnosis

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