Tests On Various Nose Configurations With Cylindrical After body In 0.3m Wind Tunnel.

摘要

Force Measurements On Four Nose Configurations With Cylindrical After body Were Performed In 0.3m Wind Tunnel In The Mach Number Range Of 0.5 To 0.8 And Angle Of Incidence -4 To 14°.From Analysis Of Aerodynamic Data, It Was Observed That The Bulbous Nose Configuration Was The Optimum Configuration With Drag Penalty.udud