| 摘要 |
Provided is a nose for a supersonic flying object, which has a natural laminar flow nose shape capable of suppressing laminar-turbulent transition and drastically reducing a frictional resistance. The nose for a supersonic flying object has a low resistive body shape symmetrical about the central axis as a basic shape, wherein the basic shape is approximately a cone shape having a linear, simple convex curve, or simple concave curve generatrix and a deformation element having a wave shape is added to the basic shape. |
