Drag reduction mechanism based on the aerospike-jet composite approach under different incoming dynamic pressures
Z Xie, C Liu, Y Meng, W Huang, Y Liang, Z Zhao - Acta Astronautica, 2024 - Elsevier
The drag experienced by the nose of an aircraft varies significantly under different incoming
flow conditions. In order to reduce the aerodynamic force on the nose of the (hypersonic) …
flow conditions. In order to reduce the aerodynamic force on the nose of the (hypersonic) …