Abstract
This paper presents a parametric and performance cycle analysis of a high performance aircraft engine using Numerical Propulsion System Simulation (NPSS). NPSS is an object oriented tool developed for the modeling and analysis of propulsion systems based on aero- thermodynamic equations. A low bypass mixed-flow turbofan engine with data for both design and off-design performance parameters available in literature is modeled in the numerical environment. The component characteristics are iterated as part of the modeling procedure. The design and off design simulations are carried out for the entire flight envelope and the performance deck is validated using the data of the modeled engine presented in the literature. The presented model may serve as a baseline for modeling and simulation of jet engines for academic and research purposes.
Original language | English |
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Title of host publication | Proceedings of 18th International Bhurban Conference on Applied Sciences and Technologies, IBCAST 2021 |
Editors | Muhammad Zafar-Uz-Zaman, Naveed A. Siddiqui, Mazhar Iqbal, Abdur Rauf, Naeem Zafar, Usman Qayyum, Tahir Jamil, Saifullah Khan, Irfan Ali, Qaisar Ahsan, Sajjad Asghar, Mureed Hussian, Shiraz Ahmad, Muhammad Rafique, Naveed Durrani, Shafiq R. Qureshi, Syed Ali Abbas, Naveed Ahsan, Abdul Mueed |
Publisher | Institute of Electrical and Electronics Engineers Inc. |
Pages | 736-741 |
Number of pages | 6 |
ISBN (Electronic) | 9780738105352 |
DOIs | |
State | Published - 12 Jan 2021 |
Externally published | Yes |
Event | 18th International Bhurban Conference on Applied Sciences and Technologies, IBCAST 2021 - Virtual, Islamabad, Pakistan Duration: 12 Jan 2021 → 16 Jan 2021 |
Publication series
Name | Proceedings of 18th International Bhurban Conference on Applied Sciences and Technologies, IBCAST 2021 |
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Conference
Conference | 18th International Bhurban Conference on Applied Sciences and Technologies, IBCAST 2021 |
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Country/Territory | Pakistan |
City | Virtual, Islamabad |
Period | 12/01/21 → 16/01/21 |
Bibliographical note
Publisher Copyright:© 2021 IEEE.
Keywords
- low bypass turbofan
- Numerical Propulsion System Simulation
- performance deck
ASJC Scopus subject areas
- Aerospace Engineering
- Industrial and Manufacturing Engineering
- Mechanical Engineering
- Ceramics and Composites
- Metals and Alloys
- Polymers and Plastics
- Surfaces, Coatings and Films