دورية أكاديمية
Effect of intermediate aerodisk mounted sharp tip spike on the drag reduction over a hemispherical body at Mach 2.0
العنوان: | Effect of intermediate aerodisk mounted sharp tip spike on the drag reduction over a hemispherical body at Mach 2.0 |
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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 |
تدمد: | 14512092 2406128X |
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