Model Identification of Unsteady Aerodynamic Loading of Delta Wings for High Angle of Attack
A Master of Science thesis in Mechatronics Submitted to the School of Engineering by Mohammad Al-Khedher, "Model Identification of Unsteady Aerodynamic Loading of Delta Wings for High Angle of Attack," June 2004. Chair of Thesis Committee Dr. Ameen Al-Jarrah & Co-Advisor Dr. Khaled Ass...
محفوظ في:
| المؤلف الرئيسي: | |
|---|---|
| التنسيق: | doctoralThesis |
| منشور في: |
2004
|
| الموضوعات: | |
| الوصول للمادة أونلاين: | http://hdl.handle.net/11073/99 |
| الوسوم: |
إضافة وسم
لا توجد وسوم, كن أول من يضع وسما على هذه التسجيلة!
|
| _version_ | 1864513434504134656 |
|---|---|
| author | Al-Khedher, Mohammad |
| author_facet | Al-Khedher, Mohammad |
| author_role | author |
| dc.contributor.none.fl_str_mv | Al Jarrah, Mohammad Amin Assaleh, Khaled |
| dc.creator.none.fl_str_mv | Al-Khedher, Mohammad |
| dc.date.none.fl_str_mv | 2004-06 2011-03-10T12:43:53Z 2011-03-10T12:43:53Z |
| dc.format.none.fl_str_mv | application/pdf |
| dc.identifier.none.fl_str_mv | 35.232-2004.02 http://hdl.handle.net/11073/99 |
| dc.language.none.fl_str_mv | en_US |
| dc.subject.none.fl_str_mv | Mechatronics Airplanes Turbojet engines Control Aerodynamics |
| dc.title.none.fl_str_mv | Model Identification of Unsteady Aerodynamic Loading of Delta Wings for High Angle of Attack |
| dc.type.none.fl_str_mv | info:eu-repo/semantics/publishedVersion info:eu-repo/semantics/doctoralThesis |
| description | A Master of Science thesis in Mechatronics Submitted to the School of Engineering by Mohammad Al-Khedher, "Model Identification of Unsteady Aerodynamic Loading of Delta Wings for High Angle of Attack," June 2004. Chair of Thesis Committee Dr. Ameen Al-Jarrah & Co-Advisor Dr. Khaled Assaleh. Thesis available only in hard copy in Reference and AUS Archives. |
| format | doctoralThesis |
| id | aus_1cc112718f2e2f9f1c25e04c97ee2cdc |
| identifier_str_mv | 35.232-2004.02 |
| language_invalid_str_mv | en_US |
| network_acronym_str | aus |
| network_name_str | aus |
| oai_identifier_str | oai:repository.aus.edu:11073/99 |
| publishDate | 2004 |
| repository.mail.fl_str_mv | |
| repository.name.fl_str_mv | |
| repository_id_str | |
| spelling | Model Identification of Unsteady Aerodynamic Loading of Delta Wings for High Angle of AttackAl-Khedher, MohammadMechatronicsAirplanesTurbojet enginesControlAerodynamicsA Master of Science thesis in Mechatronics Submitted to the School of Engineering by Mohammad Al-Khedher, "Model Identification of Unsteady Aerodynamic Loading of Delta Wings for High Angle of Attack," June 2004. Chair of Thesis Committee Dr. Ameen Al-Jarrah & Co-Advisor Dr. Khaled Assaleh. Thesis available only in hard copy in Reference and AUS Archives.College of EngineeringMultidisciplinary ProgramsMaster of Science in Mechatronics Engineering (MSMTR)Al Jarrah, Mohammad AminAssaleh, Khaled2011-03-10T12:43:53Z2011-03-10T12:43:53Z2004-06info:eu-repo/semantics/publishedVersioninfo:eu-repo/semantics/doctoralThesisapplication/pdf35.232-2004.02http://hdl.handle.net/11073/99en_USoai:repository.aus.edu:11073/992025-11-11T07:05:36Z |
| spellingShingle | Model Identification of Unsteady Aerodynamic Loading of Delta Wings for High Angle of Attack Al-Khedher, Mohammad Mechatronics Airplanes Turbojet engines Control Aerodynamics |
| status_str | publishedVersion |
| title | Model Identification of Unsteady Aerodynamic Loading of Delta Wings for High Angle of Attack |
| title_full | Model Identification of Unsteady Aerodynamic Loading of Delta Wings for High Angle of Attack |
| title_fullStr | Model Identification of Unsteady Aerodynamic Loading of Delta Wings for High Angle of Attack |
| title_full_unstemmed | Model Identification of Unsteady Aerodynamic Loading of Delta Wings for High Angle of Attack |
| title_short | Model Identification of Unsteady Aerodynamic Loading of Delta Wings for High Angle of Attack |
| title_sort | Model Identification of Unsteady Aerodynamic Loading of Delta Wings for High Angle of Attack |
| topic | Mechatronics Airplanes Turbojet engines Control Aerodynamics |
| url | http://hdl.handle.net/11073/99 |