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 drag. The nose for a supersonic flying object has a low resistive body shape symmetrical about a central axis as a base shape, wherein the base shape is approximately a cone shape having a linear, simple convex curve, or simple concave curve generatrix and a deformation element having a wavy shape is added to the base shape.
NOSE FOR SUPERSONIC FLYING OBJECT
NASE FÜR ÜBERSCHALLFLUGKÖRPER
NEZ POUR OBJET VOLANT SUPERSONIQUE
2017-01-11
Patent
Elektronische Ressource
Englisch
Supersonic ejectable-nose escape capsule
Engineering Index Backfile | 1961
|Nose section for a flying machine and associated flying machine
Europäisches Patentamt | 2019
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