Effect of intermediate aerodisk mounted sharp tip spike on the drag reduction over a hemispherical body at Mach 2.0
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 Mac...
Main Authors: | , , |
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Format: | Article |
Language: | English |
Published: |
University of Belgrade - Faculty of Mechanical Engineering, Belgrade
2020-01-01
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Series: | FME Transactions |
Subjects: | |
Online Access: | https://scindeks-clanci.ceon.rs/data/pdf/1451-2092/2020/1451-20922004779T.pdf |