Academic Journal

Morphing Winglet Design for Aerodynamic Performance Optimization of the CRJ-700 Aircraft. Part 1 – Structural Design

التفاصيل البيبلوغرافية
العنوان: Morphing Winglet Design for Aerodynamic Performance Optimization of the CRJ-700 Aircraft. Part 1 – Structural Design
المؤلفون: Paul MEYRAN, Hugo PAIN, Ruxandra Mihaela BOTEZ, Jeremy LALIBERTÉ
المصدر: INCAS Bulletin, Vol 13, Iss 4, Pp 113-128 (2021)
بيانات النشر: National Institute for Aerospace Research “Elie Carafoli” - INCAS, 2021.
سنة النشر: 2021
المجموعة: LCC:Motor vehicles. Aeronautics. Astronautics
مصطلحات موضوعية: design, morphing winglet, aerodynamics, structure, optimization, Motor vehicles. Aeronautics. Astronautics, TL1-4050
الوصف: This study aims to design a morphing winglet structure for the CRJ-700 regional transport aircraft. The morphing technology is applied on winglets to demonstrate a significant increase of the aerodynamic performance of aircraft. From the aerodynamic data of the LARCASE Virtual Research Simulator VRESIM, the aerodynamic benefits in the cruising phase were obtained through a study on the ParaView software. The morphing winglet design was drawn using CATIA V5; this new concept included several structural components, as well as a simple and light mechanism allowing to orientate the winglet angles between 90° and -90° of inclination. The structural model was exported to HyperMesh structural analysis software. Maximum stresses were obtained, and the model demonstrated its resistance to maximum aerodynamic loads as well as load factors of -2G to 7G.
نوع الوثيقة: article
وصف الملف: electronic resource
اللغة: English
تدمد: 2066-8201
2247-4528
Relation: https://bulletin.incas.ro/files/meyran_pain_botez_laliberte_part_1_vol_13_iss_4.pdf; https://doaj.org/toc/2066-8201; https://doaj.org/toc/2247-4528
DOI: 10.13111/2066-8201.2021.13.4.10
URL الوصول: https://doaj.org/article/b1f17bde6a2c4c05a50cb0fc0541cea1
رقم الانضمام: edsdoj.b1f17bde6a2c4c05a50cb0fc0541cea1
قاعدة البيانات: Directory of Open Access Journals
الوصف
تدمد:20668201
22474528
DOI:10.13111/2066-8201.2021.13.4.10