• Sharang Ahirekar
• Joshua Kumar Takri
• Prabhjot Singh
• Ashwani Kumar
• Manikandan S

Contemporarily, innumerable technologies are being brought into operation for missile maneuverings. By the same token, this research provides a substitute as well an advanced tactic to the habitual tack of maneuvering missiles in which the reaction thrusters and the control surfaces installed on it has been utilized. Here, a force which is proportional to the crosswind direction and the flight path of a particular missile is journeyed on neutralizing the same with regards to its spin and geometry running under a unique velocity level. The force encountered by the missile is further named as the Magnus Force moreover the same force may also be applied for future maneuverings. In addition to this, it is observed that in absence of the Magnus Force in gyrating missiles, there exists an identical RPM. This paper ascertains the condition where no Magnus Fore occurs in the missile i.e. stable/equilibrium state; into the bargain, by commuting the swivel from the stable condition it also points out the Magnus Force.

Spin Neutralization, Magnus Force, crosswind conditions, Missile Maneuvering

"Determination of maneuvering force on spin stabilized missile based on Magnus effect under subsonic flow conditions", International Journal of Emerging Technologies and Innovative Research (www.jetir.org), ISSN:2349-5162, Vol.8, Issue 5, page no.b290-b296, May-2021, Available :http://www.jetir.org/papers/JETIR2105168.pdf

"Determination of maneuvering force on spin stabilized missile based on Magnus effect under subsonic flow conditions", International Journal of Emerging Technologies and Innovative Research (www.jetir.org | UGC and issn Approved), ISSN:2349-5162, Vol.8, Issue 5, page no. ppb290-b296, May-2021, Available at : http://www.jetir.org/papers/JETIR2105168.pdf