Transaint Simulation of Turbojet Engine With Hybrid Method

Please enable javascript in your browser.

Moradifar, Keyvan | 2011

860 Viewed

Type of Document: M.Sc. Thesis
Language: Farsi
Document No: 42685 (45)
University: Sharif University of Technology
Department: Aerospace Engineering
Advisor(s): Ghorbanian, Kaveh
Abstract:
According to importance for modeling engine in propulsion subject and delecacies and complenity of this topic. Modeling turbofan engine has been chosen as the target of this project.Three methods are presented by this modeling and the results are compared. In addition, problems and shortcomings of each method are surveyed and stated. Surveying of each method is done step by step. In order to simplify description for any reader to reach the ultimate goal .In the beginning of the process, each coded method is stated full description .furthermore modeling process is illuminated. More ever, difference in methods is expressed. The results of three methods are processed and presented completely. Finally, some new suggestions re presented
Keywords:
Transition State ; Turbojet ; Hybrid Methods ; Real-Time Simulation ; Intercomponent Volume Method

No TOC