• Kakarla Devi Prasanna
• Rakesh S

When the fluid velocity is much larger than the velocity of sound in the flow field(M>1.2, M<5) is supersonic flow. When the vehicle is moving faster than the speed of sound Shock waves will occur which makes bombs have more chances of explosion. If the shock wave moves much faster than the energy of the bomb, fades away quickly. Increasing the shock wave on the surface and improving the interaction between shock wave and boundary layer will design the nose part of the re-entry vehicle. Designing the nose part (Blunted double-cone configuration) for a Re-entry vehicle and analysing by including the Magnus effect over the blunted double-cone configuration in the region of the Shock wave boundary layer interaction (SBLI) in supersonic condition considering (M=3). To obtain the better interaction between shock wave and boundary layer by involving the spinning effect over the surface and analysing the result through computational fluid dynamics (CFD). Considering the result of spinning effect over the blunted double cone and comparing the result with without spinning effect over the blunted double-cone configuration through CFD to provide the data that attain in an efficient manner. Determining the result to attain minimum drag, surface temperature and other factors act on the nose part while re-entering into the atmosphere. Determining the result to attain maximum efficiency, minimizing bombs, and comparing the result through CFD.

Shock wave, Boundary layer, SBLI, Magnus effect, Supersonic flow, CFD.

" Design and Analysis of Nose part for Re-entry vehicle considering Magnus effect over the Blunted Double Cone Configuration in the region of the Shock Wave Boundary Layer Interaction. ", International Journal of Emerging Technologies and Innovative Research (www.jetir.org), ISSN:2349-5162, Vol.9, Issue 4, page no.b287-b294, April-2022, Available :http://www.jetir.org/papers/JETIR2204137.pdf

" Design and Analysis of Nose part for Re-entry vehicle considering Magnus effect over the Blunted Double Cone Configuration in the region of the Shock Wave Boundary Layer Interaction. ", International Journal of Emerging Technologies and Innovative Research (www.jetir.org | UGC and issn Approved), ISSN:2349-5162, Vol.9, Issue 4, page no. ppb287-b294, April-2022, Available at : http://www.jetir.org/papers/JETIR2204137.pdf