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Title: :  INVESTIGATION OF HEMISPHERICAL AEROSPIKE FOR BLUNT BODY AT HYPERSONIC SPEED
PaperId: :  20188
Published in:   International Journal Of Advance Research And Innovative Ideas In Education
Publisher:   IJARIIE
e-ISSN:   2395-4396
Volume/Issue:    Volume 9 Issue 3 2023
DUI:    16.0415/IJARIIE-20188
Licence: :   IJARIIE is licensed under a Creative Commons Attribution-ShareAlike 4.0 International License.

Author NameAuthor Institute
Aditya Shirolkar RNS Institute of Technology
Charu Chandra CRNS Institute of Technology
Dheemanth B A RNS Institute of Technology
Yash Vimalesh Revankar RNS Institute of Technology
Mahesh Kumar NRNS Institute of Technology
Chethana S Batakurki RNS Institute of Technology

Abstract

Computational Fluid Dynamics
aero-spike, blunt cone nose, aerodynamic drag, bow shock
Aerospace vehicles, such as re-entry vehicles, satellite launching vehicles, missiles, and rockets, operate at extremely high speeds, leading to the generation of shock waves and significant heat and drag. The high heat and drag generation significantly affect the efficiency and maneuverability of such vehicles. To counter this, the present study focuses on the design and analysis of drag reduction techniques for hypersonic vehicles, specifically investigating the effectiveness of different spikes with hemispherical aerodisk. The blunt body configuration is employed as a model, and the analysis is conducted at a hypersonic speed corresponding to Mach number 6. The research explores the impact of varying sizes of spiked blunt bodies, considering the length of the spike to diameter of the blunt body (L/D) ratios of 1.5 and 2. The introduction of a front-facing spike effectively reduces the intensity of the bow shock at the front part of the blunt body by converting it to an oblique shock wave. Notably, a drag reduction of 60% is achieved using a spike with an L/D ratio of 1.5, while a higher reduction of 75% is attained with an L/D ratio of 2. Additionally, the study examines the influence of altering the minor radius of the aerodisk, further evaluating its effect on reduction of the shock wave formation in the frontal region of the aerospike. The findings highlight the potential of these drag reduction techniques to enhance the aerodynamic performance of hypersonic aerospace vehicles, paving the way for improved efficiency and maneuverability in high-speed flight conditions.

Citations

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IJARIIE Aditya Shirolkar , Charu Chandra C, Dheemanth B A , Yash Vimalesh Revankar , Mahesh Kumar N, and Chethana S Batakurki . "INVESTIGATION OF HEMISPHERICAL AEROSPIKE FOR BLUNT BODY AT HYPERSONIC SPEED" International Journal Of Advance Research And Innovative Ideas In Education Volume 9 Issue 3 2023 Page 982-993
MLA Aditya Shirolkar , Charu Chandra C, Dheemanth B A , Yash Vimalesh Revankar , Mahesh Kumar N, and Chethana S Batakurki . "INVESTIGATION OF HEMISPHERICAL AEROSPIKE FOR BLUNT BODY AT HYPERSONIC SPEED." International Journal Of Advance Research And Innovative Ideas In Education 9.3(2023) : 982-993.
APA Aditya Shirolkar , Charu Chandra C, Dheemanth B A , Yash Vimalesh Revankar , Mahesh Kumar N, & Chethana S Batakurki . (2023). INVESTIGATION OF HEMISPHERICAL AEROSPIKE FOR BLUNT BODY AT HYPERSONIC SPEED. International Journal Of Advance Research And Innovative Ideas In Education, 9(3), 982-993.
Chicago Aditya Shirolkar , Charu Chandra C, Dheemanth B A , Yash Vimalesh Revankar , Mahesh Kumar N, and Chethana S Batakurki . "INVESTIGATION OF HEMISPHERICAL AEROSPIKE FOR BLUNT BODY AT HYPERSONIC SPEED." International Journal Of Advance Research And Innovative Ideas In Education 9, no. 3 (2023) : 982-993.
Oxford Aditya Shirolkar , Charu Chandra C, Dheemanth B A , Yash Vimalesh Revankar , Mahesh Kumar N, and Chethana S Batakurki . 'INVESTIGATION OF HEMISPHERICAL AEROSPIKE FOR BLUNT BODY AT HYPERSONIC SPEED', International Journal Of Advance Research And Innovative Ideas In Education, vol. 9, no. 3, 2023, p. 982-993. Available from IJARIIE, https://ijariie.com/AdminUploadPdf/INVESTIGATION_OF_HEMISPHERICAL_AEROSPIKE_FOR_BLUNT_BODY_AT_HYPERSONIC_SPEED_ijariie20188.pdf (Accessed : ).
Harvard Aditya Shirolkar , Charu Chandra C, Dheemanth B A , Yash Vimalesh Revankar , Mahesh Kumar N, and Chethana S Batakurki . (2023) 'INVESTIGATION OF HEMISPHERICAL AEROSPIKE FOR BLUNT BODY AT HYPERSONIC SPEED', International Journal Of Advance Research And Innovative Ideas In Education, 9(3), pp. 982-993IJARIIE [Online]. Available at: https://ijariie.com/AdminUploadPdf/INVESTIGATION_OF_HEMISPHERICAL_AEROSPIKE_FOR_BLUNT_BODY_AT_HYPERSONIC_SPEED_ijariie20188.pdf (Accessed : )
IEEE Aditya Shirolkar , Charu Chandra C, Dheemanth B A , Yash Vimalesh Revankar , Mahesh Kumar N, and Chethana S Batakurki , "INVESTIGATION OF HEMISPHERICAL AEROSPIKE FOR BLUNT BODY AT HYPERSONIC SPEED," International Journal Of Advance Research And Innovative Ideas In Education, vol. 9, no. 3, pp. 982-993, May-Jun 2023. [Online]. Available: https://ijariie.com/AdminUploadPdf/INVESTIGATION_OF_HEMISPHERICAL_AEROSPIKE_FOR_BLUNT_BODY_AT_HYPERSONIC_SPEED_ijariie20188.pdf [Accessed : ].
Turabian Aditya Shirolkar , Charu Chandra C, Dheemanth B A , Yash Vimalesh Revankar , Mahesh Kumar N, and Chethana S Batakurki . "INVESTIGATION OF HEMISPHERICAL AEROSPIKE FOR BLUNT BODY AT HYPERSONIC SPEED." International Journal Of Advance Research And Innovative Ideas In Education [Online]. volume 9 number 3 ().
Vancouver Aditya Shirolkar , Charu Chandra C, Dheemanth B A , Yash Vimalesh Revankar , Mahesh Kumar N, and Chethana S Batakurki . INVESTIGATION OF HEMISPHERICAL AEROSPIKE FOR BLUNT BODY AT HYPERSONIC SPEED. International Journal Of Advance Research And Innovative Ideas In Education [Internet]. 2023 [Cited : ]; 9(3) : 982-993. Available from: https://ijariie.com/AdminUploadPdf/INVESTIGATION_OF_HEMISPHERICAL_AEROSPIKE_FOR_BLUNT_BODY_AT_HYPERSONIC_SPEED_ijariie20188.pdf
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