Sensitivity and Design Point Analysis of RD-93 Engine at Static Sea Level using Numerical Propulsion System Simulation

Maria Sadaf, M. Kamran Zeb, Shuaib Salamat, Messam Abbas Naqvi

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

1 Scopus citations

Abstract

The design and prototyping of jet engines is an extremely costly and laborious task. An alternative to at this is the development of variants of existing engines for enhanced performance which requires detailed modeling of engine in mathematical environment for precise evaluation of performance parameters. This paper presents mathematical modelling and sensitivity analysis of performance of RD-93, a low bypass turbofan engine, towards design parameters including pressure ratio of turbomachinery components, bypass ratio and critical temperatures. The effect of varying the efficiency of engine components on performance of overall engine is estimated using numerical environment of Numerical Propulsion System Simulation (NPSS). The results of performed analysis can serve as a guide for further parametric cycle analyses of low bypass turbofan engines.

Original languageEnglish
Title of host publication2020 3rd International Conference on Computing, Mathematics and Engineering Technologies
Subtitle of host publicationIdea to Innovation for Building the Knowledge Economy, iCoMET 2020
PublisherInstitute of Electrical and Electronics Engineers Inc.
ISBN (Electronic)9781728149707
DOIs
StatePublished - Jan 2020
Externally publishedYes
Event3rd International Conference on Computing, Mathematics and Engineering Technologies, iCoMET 2020 - Sukkur, Pakistan
Duration: 29 Jan 202030 Jan 2020

Publication series

Name2020 3rd International Conference on Computing, Mathematics and Engineering Technologies: Idea to Innovation for Building the Knowledge Economy, iCoMET 2020

Conference

Conference3rd International Conference on Computing, Mathematics and Engineering Technologies, iCoMET 2020
Country/TerritoryPakistan
CitySukkur
Period29/01/2030/01/20

Bibliographical note

Publisher Copyright:
© 2020 IEEE.

Keywords

  • bypass ratio
  • low bypass turbofan
  • mathematical modelling
  • numerical propulsion system simulation
  • pressure ratio

ASJC Scopus subject areas

  • Computer Networks and Communications
  • Computer Science Applications
  • Information Systems and Management
  • Energy Engineering and Power Technology
  • Renewable Energy, Sustainability and the Environment
  • Management, Monitoring, Policy and Law
  • Computational Mathematics
  • Control and Optimization

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