Dynamical Torsional Analysis of Schweizer 300C Helicopter Rotor Systems
The study in this research focuses on building simulation model the motion systems of Schweizer 300C helicopter and Emphasises is put on examine the most suitable simulation techniques used to deal with the most accurate and closest to reality dynamical torsional response of the motion systems which...
محفوظ في:
| المؤلف الرئيسي: | |
|---|---|
| منشور في: |
2019
|
| الموضوعات: | |
| الوصول للمادة أونلاين: | https://bspace.buid.ac.ae/handle/1234/1421 |
| الوسوم: |
إضافة وسم
لا توجد وسوم, كن أول من يضع وسما على هذه التسجيلة!
|
| _version_ | 1862980613079826432 |
|---|---|
| author | AL-SAEEDI, HAITHAM KHAMIS MOHAMMED |
| author_facet | AL-SAEEDI, HAITHAM KHAMIS MOHAMMED |
| author_role | author |
| dc.creator.none.fl_str_mv | AL-SAEEDI, HAITHAM KHAMIS MOHAMMED |
| dc.date.none.fl_str_mv | 2019-06-23T10:42:29Z 2019-06-23T10:42:29Z 2019-01 |
| dc.format.none.fl_str_mv | application/pdf |
| dc.identifier.none.fl_str_mv | 2015215185 https://bspace.buid.ac.ae/handle/1234/1421 |
| dc.language.none.fl_str_mv | en |
| dc.publisher.none.fl_str_mv | The British University in Dubai (BUiD) |
| dc.subject.none.fl_str_mv | Helicopter Rotor Systems Schweizer 300C helicopter modeling techniques Distributed-Lumped Parameter technique (DLPMT) |
| dc.title.none.fl_str_mv | Dynamical Torsional Analysis of Schweizer 300C Helicopter Rotor Systems |
| dc.type.none.fl_str_mv | Dissertation |
| description | The study in this research focuses on building simulation model the motion systems of Schweizer 300C helicopter and Emphasises is put on examine the most suitable simulation techniques used to deal with the most accurate and closest to reality dynamical torsional response of the motion systems which will lead to the best analysis. In The first part of this research, an introductory to the history of helicopters and their dynamic fundamentles and the development and expansion of the Modeling methods from the beginning to the current forms adopted for wide variety engineering system applications. The problem identified examines the chances and possibilities of simulating the motion systems (tail and main rotors) of Schweizer 300C helicopter .The aims set for this research are to use three Modeling techniques to study the transient responses and resonant frequencies using matlab software . In this research three different techniques were adopted and compared for the simulation of the movement system of this heilcopter to identify the best and most accurate representation of dynamic torsional analysis of motion systems. The Modeling techniques used in this research are the Lumped Parameter Modeling-LPM, Finite Element Method-FEM and the Distributed-Lumped Parameter (Hybrid) model-DLPM. Finally, Modeling techniques and results obtained from each technique are compared and it can be concluded that Distributed-Lumped Parameter technique (DLPMT) is the most accurate and closest to the reality for this and such applications. |
| id | budr_f46b02b30305337dbd0d169d54c9a806 |
| identifier_str_mv | 2015215185 |
| language_invalid_str_mv | en |
| network_acronym_str | budr |
| network_name_str | The British University in Dubai repository |
| oai_identifier_str | oai:bspace.buid.ac.ae:1234/1421 |
| publishDate | 2019 |
| publisher.none.fl_str_mv | The British University in Dubai (BUiD) |
| repository.mail.fl_str_mv | |
| repository.name.fl_str_mv | |
| repository_id_str | |
| spelling | Dynamical Torsional Analysis of Schweizer 300C Helicopter Rotor SystemsAL-SAEEDI, HAITHAM KHAMIS MOHAMMEDHelicopter Rotor SystemsSchweizer 300C helicoptermodeling techniquesDistributed-Lumped Parameter technique (DLPMT)The study in this research focuses on building simulation model the motion systems of Schweizer 300C helicopter and Emphasises is put on examine the most suitable simulation techniques used to deal with the most accurate and closest to reality dynamical torsional response of the motion systems which will lead to the best analysis. In The first part of this research, an introductory to the history of helicopters and their dynamic fundamentles and the development and expansion of the Modeling methods from the beginning to the current forms adopted for wide variety engineering system applications. The problem identified examines the chances and possibilities of simulating the motion systems (tail and main rotors) of Schweizer 300C helicopter .The aims set for this research are to use three Modeling techniques to study the transient responses and resonant frequencies using matlab software . In this research three different techniques were adopted and compared for the simulation of the movement system of this heilcopter to identify the best and most accurate representation of dynamic torsional analysis of motion systems. The Modeling techniques used in this research are the Lumped Parameter Modeling-LPM, Finite Element Method-FEM and the Distributed-Lumped Parameter (Hybrid) model-DLPM. Finally, Modeling techniques and results obtained from each technique are compared and it can be concluded that Distributed-Lumped Parameter technique (DLPMT) is the most accurate and closest to the reality for this and such applications.The British University in Dubai (BUiD)2019-06-23T10:42:29Z2019-06-23T10:42:29Z2019-01Dissertationapplication/pdf2015215185https://bspace.buid.ac.ae/handle/1234/1421enoai:bspace.buid.ac.ae:1234/14212021-09-16T13:17:51Z |
| spellingShingle | Dynamical Torsional Analysis of Schweizer 300C Helicopter Rotor Systems AL-SAEEDI, HAITHAM KHAMIS MOHAMMED Helicopter Rotor Systems Schweizer 300C helicopter modeling techniques Distributed-Lumped Parameter technique (DLPMT) |
| title | Dynamical Torsional Analysis of Schweizer 300C Helicopter Rotor Systems |
| title_full | Dynamical Torsional Analysis of Schweizer 300C Helicopter Rotor Systems |
| title_fullStr | Dynamical Torsional Analysis of Schweizer 300C Helicopter Rotor Systems |
| title_full_unstemmed | Dynamical Torsional Analysis of Schweizer 300C Helicopter Rotor Systems |
| title_short | Dynamical Torsional Analysis of Schweizer 300C Helicopter Rotor Systems |
| title_sort | Dynamical Torsional Analysis of Schweizer 300C Helicopter Rotor Systems |
| topic | Helicopter Rotor Systems Schweizer 300C helicopter modeling techniques Distributed-Lumped Parameter technique (DLPMT) |
| url | https://bspace.buid.ac.ae/handle/1234/1421 |