Shyam Singh Kanwar. Numerical Investigation of Flow Modification Cooling Technique to Mitigate Aerodynamic Heating and Wave Drag in Hypersonic Flows of 60^0 Blunted Cones. IJM [Internet]. 2023Dec.31 [cited 2026Jan.10];17(4):561 - 577. Available from: https://themultiphysicsjournal.com/index.php/ijm/article/view/2081