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Effect of a Circular Ring on the Side Force of a Cone-Cylinder Body

Authors :
Sudip Das
P. Kumar
Shashank Gaurav
Source :
Journal of Aerospace Technology and Management, Volume: 12, Article number: e0620, Published: 13 MAR 2020, Journal of Aerospace Technology and Management v.12 2020, Journal of Aerospace Technology and Management, Departamento de Ciência e Tecnologia Aeroespacial (DCTA), instacron:DCTA, Journal of Aerospace Technology and Management, Vol 12, Iss 1, Pp 0612-0612 (2020)
Publication Year :
2020
Publisher :
FapUNIFESP (SciELO), 2020.

Abstract

This paper aims to investigate the side force on a cone-cylinder geometry at different angles of attack (α) by adopting experiments and computations. The cone-cylinder configuration had a length to diameter ratio (L/D) of 10, and a base diameter (D) of 25 mm. The nose shape had a fineness ratio of approximately 3. Results indicated that the side force increases with the increasing of the angle of attack. A circular ring was used to reduce the side force at different angles of attack. Using a smaller height ring (2% of local diameter) in the initial portion of the body did not reduce the side force significantly at lower angles of attack. However, a ring with larger height (5% of local diameter) placed at 2.5 times the diameter of the body from the tip reduced the side force at almost all the angles of attack.

Details

ISSN :
21759146
Database :
OpenAIRE
Journal :
Journal of Aerospace Technology and Management
Accession number :
edsair.doi.dedup.....6258234357840d6e9bcd9e179d427749
Full Text :
https://doi.org/10.5028/jatm.v12.1096