دورية أكاديمية

Effect of intermediate aerodisk mounted sharp tip spike on the drag reduction over a hemispherical body at Mach 2.0

التفاصيل البيبلوغرافية
العنوان: Effect of intermediate aerodisk mounted sharp tip spike on the drag reduction over a hemispherical body at Mach 2.0
المؤلفون: Tembhurnikar Payal V., Jadhav Akash T., Sahoo Devabrata
المصدر: FME Transactions, Vol 48, Iss 4, Pp 779-786 (2020)
بيانات النشر: University of Belgrade - Faculty of Mechanical Engineering, Belgrade, 2020.
سنة النشر: 2020
المجموعة: LCC:Engineering (General). Civil engineering (General)
LCC:Mechanics of engineering. Applied mechanics
مصطلحات موضوعية: supersonic flow, drag reduction, spike, aerodisk, Engineering (General). Civil engineering (General), TA1-2040, Mechanics of engineering. Applied mechanics, TA349-359
الوصف: Reduction of forebody drag in high speed flying vehicles such as rockets and missiles are of high research interest in the present time. In the present research, drag reduction obtained by using an intermediate aerodisk mounted sharp tip spike has been investigated using computational studies at Mach number of 2.0. The flowfield over a hemispherical blunt body with an intermediate aerodisk mounted sharp tip spike is investigated at zero degree angle of attack and the amount of drag reduction obtained is then compared with that of a conventional sharp tip spike mounted hemisphere. The presence of an intermediate aerodisk changes the flow physics and shock system over the blunt body. The change in the system of shock waves by mounting an intermediate aerodisk results in a higher percentage (20% higher) of drag reduction generated by the blunt spiked body moving at a supersonic speed of Mach 2.0. Use of intermediate aerodisk proves to be beneficial in terms of drag reduction for spike lengths ranging beyond the critical length.
نوع الوثيقة: article
وصف الملف: electronic resource
اللغة: English
تدمد: 1451-2092
2406-128X
العلاقة: https://scindeks-clanci.ceon.rs/data/pdf/1451-2092/2020/1451-20922004779T.pdfTest; https://doaj.org/toc/1451-2092Test; https://doaj.org/toc/2406-128XTest
الوصول الحر: https://doaj.org/article/9735f00949f7479cb6b6d52d86e96568Test
رقم الانضمام: edsdoj.9735f00949f7479cb6b6d52d86e96568
قاعدة البيانات: Directory of Open Access Journals