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General parameters used for constructing nose cone profiles. Given the problem of the aerodynamic design of the nose cone section of any vehicle or body meant to travel through a compressible fluid medium (such as a rocket or aircraft, missile, shell or bullet), an important problem is the determination of the nose cone geometrical shape for optimum performance.
Date/Time Thumbnail Dimensions User Comment; current: 16:57, 27 December 2013: 1,500 × 1,000 (28 KB): Andersenman: Added grid lines as well as another graph for C=1.333.
The droop nose is a feature fitted to a small number of aircraft types so the nose of the aircraft can be lowered during takeoff and landing to improve the pilot's view of the ground below. This feature is used with a very-low aspect ratio wing such as a delta wing .
Date/Time Thumbnail Dimensions User Comment; current: 16:59, 27 December 2013: 1,500 × 1,000 (25 KB): Andersenman: Changed format slightly to make it wider, and adjusted the key texts.
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A nose cone is the conically shaped forwardmost section of a rocket, guided missile or aircraft, designed to modulate oncoming airflow behaviors and minimize aerodynamic drag. Nose cones are also designed for submerged watercraft such as submarines , submersibles and torpedoes , and in high-speed land vehicles such as rocket cars and velomobiles .