Implications of a Military Turbofan's High-Pressure Turbine Erosion for Blade's Creep Life-Consumption-Reference-Cited by-同舟云学术

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Implications of a Military Turbofan's High-Pressure Turbine Erosion for Blade's Creep Life-Consumption

Published:2010-01 Issue:1 Volume:26 Page:177-182
ISSN:0748-4658
Container-title:Journal of Propulsion and Power
language:en
Short-container-title:Journal of Propulsion and Power

Author:

Naeem Muhammad¹,Ul-Haq Irfan¹

Affiliation:

1. Institute of Space Technology, Islamabad 44000, Pakistan

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/10.2514/1.38828

Reference20 articles.

1. Use of Computer Simulation Techniques to Assess Thrust Rating as a Means of Reducing Turbo-Jet Life Cycle Costs

2. Impacts of aero-engine deteriorations on military aircraft mission's effectiveness

3. Impacts of low-pressure (LP) compressor’s deterioration upon an aero-engine’s high-pressure (HP) turbine blade’s life consumption

4. Impacts of low-pressure (LP) compressor’s deterioration of a turbofan engine upon fuel-usage of a military aircraft

Cited by 2 articles. 订阅此论文施引文献订阅此论文施引文献，注册后可以免费订阅5篇论文的施引文献，订阅后可以查看论文全部施引文献

1. Review on Creep Phenomenon and Its Model in Aircraft Engines;International Journal of Aerospace Engineering;2023-05-29

2. Implications of High-Pressure Turbine’s Erosion for a Military Turbofan’s Fuel Consumption;Journal of Aerospace Engineering;2012-01

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