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Title: :  Computational study of flow over Fire II Re-entry Vehicle at various Supersonic Speeds
PaperId: :  14540
Published in:   International Journal Of Advance Research And Innovative Ideas In Education
Publisher:   IJARIIE
e-ISSN:   2395-4396
Volume/Issue:    Volume 7 Issue 3 2021
DUI:    16.0415/IJARIIE-14540
Licence: :   IJARIIE is licensed under a Creative Commons Attribution-ShareAlike 4.0 International License.

Author NameAuthor Institute
Kanishka DeepakR V College of Engineering
Anish G P NandR V College of Engineering

Abstract

Aerospace Engineering
Re-entry vehicle, capsule, Supersonic flow, Computational fluid dynamics, Thermal heating, Heat flux, Shock waves, Ansys
Re-entry modules are blunt bodies that are designed in such a way that they can withstand the extreme temperature loads during atmospheric re-entry. Designing a re-entry vehicle requires dependable data on the aerodynamic flow properties. After hypersonic re-entry, the vehicle has to decelerate at supersonic speeds until the parachutes are deployed. Examining the flow properties over the vehicle at supersonic speed is important of which temperature serves as critical data for a successful recovery operation. Hence this paper is presented to understand the variation in temperature, as the re-entry vehicle decelerates from Mach no. 3 to 1.2. Temperature variation along with pressure distribution is obtained computationally for freestream Mach numbers 1.2, 2 and 3 with appropriate boundary conditions using Ansys FLUENT. The results also describe the flow field around a capsule in supersonic flow and understand the importance of shock waves which influences the aerodynamic forces on the capsule. The analysis showed the flow-field features such as bow shock wave on the frontal heat shield surface and expansion fan on the shoulder terminating region around the re-entry capsule. This research will assist spacecraft design engineers to analyse the flowfield and choose the appropriate materials. Further, the analysis performed can aid in the designing of parachutes that are used to decelerate the re-entry vehicle for a safe landing.

Citations

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IJARIIE Kanishka Deepak, and Anish G P Nand. "Computational study of flow over Fire II Re-entry Vehicle at various Supersonic Speeds" International Journal Of Advance Research And Innovative Ideas In Education Volume 7 Issue 3 2021 Page 2149-2157
MLA Kanishka Deepak, and Anish G P Nand. "Computational study of flow over Fire II Re-entry Vehicle at various Supersonic Speeds." International Journal Of Advance Research And Innovative Ideas In Education 7.3(2021) : 2149-2157.
APA Kanishka Deepak, & Anish G P Nand. (2021). Computational study of flow over Fire II Re-entry Vehicle at various Supersonic Speeds. International Journal Of Advance Research And Innovative Ideas In Education, 7(3), 2149-2157.
Chicago Kanishka Deepak, and Anish G P Nand. "Computational study of flow over Fire II Re-entry Vehicle at various Supersonic Speeds." International Journal Of Advance Research And Innovative Ideas In Education 7, no. 3 (2021) : 2149-2157.
Oxford Kanishka Deepak, and Anish G P Nand. 'Computational study of flow over Fire II Re-entry Vehicle at various Supersonic Speeds', International Journal Of Advance Research And Innovative Ideas In Education, vol. 7, no. 3, 2021, p. 2149-2157. Available from IJARIIE, https://ijariie.com/AdminUploadPdf/Computational_study_of_flow_over_Fire_II_Re_entry_Vehicle_at_various_Supersonic_Speeds_ijariie14540.pdf (Accessed : 06 June 2023).
Harvard Kanishka Deepak, and Anish G P Nand. (2021) 'Computational study of flow over Fire II Re-entry Vehicle at various Supersonic Speeds', International Journal Of Advance Research And Innovative Ideas In Education, 7(3), pp. 2149-2157IJARIIE [Online]. Available at: https://ijariie.com/AdminUploadPdf/Computational_study_of_flow_over_Fire_II_Re_entry_Vehicle_at_various_Supersonic_Speeds_ijariie14540.pdf (Accessed : 06 June 2023)
IEEE Kanishka Deepak, and Anish G P Nand, "Computational study of flow over Fire II Re-entry Vehicle at various Supersonic Speeds," International Journal Of Advance Research And Innovative Ideas In Education, vol. 7, no. 3, pp. 2149-2157, May-Jun 2021. [Online]. Available: https://ijariie.com/AdminUploadPdf/Computational_study_of_flow_over_Fire_II_Re_entry_Vehicle_at_various_Supersonic_Speeds_ijariie14540.pdf [Accessed : 06 June 2023].
Turabian Kanishka Deepak, and Anish G P Nand. "Computational study of flow over Fire II Re-entry Vehicle at various Supersonic Speeds." International Journal Of Advance Research And Innovative Ideas In Education [Online]. volume 7 number 3 (06 June 2023).
Vancouver Kanishka Deepak, and Anish G P Nand. Computational study of flow over Fire II Re-entry Vehicle at various Supersonic Speeds. International Journal Of Advance Research And Innovative Ideas In Education [Internet]. 2021 [Cited : 06 June 2023]; 7(3) : 2149-2157. Available from: https://ijariie.com/AdminUploadPdf/Computational_study_of_flow_over_Fire_II_Re_entry_Vehicle_at_various_Supersonic_Speeds_ijariie14540.pdf
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