دورية أكاديمية

A Generic Model for Benchmark Aerodynamic Analysis of Fifth-Generation High-Performance Aircraft

التفاصيل البيبلوغرافية
العنوان: A Generic Model for Benchmark Aerodynamic Analysis of Fifth-Generation High-Performance Aircraft
المؤلفون: Nicholas F. Giannelis, Tamas Bykerk, Gareth A. Vio
المصدر: Aerospace, Vol 10, Iss 9, p 746 (2023)
بيانات النشر: MDPI AG, 2023.
سنة النشر: 2023
المجموعة: LCC:Motor vehicles. Aeronautics. Astronautics
مصطلحات موضوعية: high angle of attack aerodynamics, delta-wings, vortical flows, computational fluid dynamics, experimental aerodynamics, benchmark aerodynamic models, Motor vehicles. Aeronautics. Astronautics, TL1-4050
الوصف: This paper introduces a generic model for the study of aerodynamic behaviour relevant to fifth-generation high-performance aircraft. The model design is presented, outlining simplifications made to retain the key features of modern high-performance vehicles while ensuring a manufacturable geometry. Subsonic wind tunnel tests were performed with force and moment balance measurements used to develop a database of experimental validation data for the platform at a freestream velocity of 20 m/s. Numerical simulations are also presented and validated by the experiments and further employed to ensure the vortex behaviour is consistent with contemporary high-performance platforms. A sensitivity study of the computational predictions from the turbulence modelling approach is also presented. This geometry is the first in a suite of representative aircraft geometries (the Sydney Standard Aerodynamic Models), in which all geometries, computational models, and experimental data are made openly available to the research community (accessible via this link: https://zenodo.org/communities/ssam_gen5Test/) to serve as validation test cases and promote best practices in aerodynamic modelling.
نوع الوثيقة: article
وصف الملف: electronic resource
اللغة: English
تدمد: 10090746
2226-4310
العلاقة: https://www.mdpi.com/2226-4310/10/9/746Test; https://doaj.org/toc/2226-4310Test
DOI: 10.3390/aerospace10090746
الوصول الحر: https://doaj.org/article/8add2cf1ec6f4334b972047f4ca2282aTest
رقم الانضمام: edsdoj.8add2cf1ec6f4334b972047f4ca2282a
قاعدة البيانات: Directory of Open Access Journals
الوصف
تدمد:10090746
22264310
DOI:10.3390/aerospace10090746