Methodology for Development of Complete Engine Deck for a Low Bypass Turbofan Engine

Sabih Sajjad Ahmed, Muhammad Kamran Zeb, Shuaib Salamat

Research output: Chapter in Book/Report/Conference proceedingConference contributionpeer-review

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 languageEnglish
Title of host publicationProceedings of 18th International Bhurban Conference on Applied Sciences and Technologies, IBCAST 2021
EditorsMuhammad 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
PublisherInstitute of Electrical and Electronics Engineers Inc.
Pages736-741
Number of pages6
ISBN (Electronic)9780738105352
DOIs
StatePublished - 12 Jan 2021
Externally publishedYes
Event18th International Bhurban Conference on Applied Sciences and Technologies, IBCAST 2021 - Virtual, Islamabad, Pakistan
Duration: 12 Jan 202116 Jan 2021

Publication series

NameProceedings of 18th International Bhurban Conference on Applied Sciences and Technologies, IBCAST 2021

Conference

Conference18th International Bhurban Conference on Applied Sciences and Technologies, IBCAST 2021
Country/TerritoryPakistan
CityVirtual, Islamabad
Period12/01/2116/01/21

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

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