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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.
A drag-reducing aerospike is a device (see nose cone design) used to reduce the forebody pressure aerodynamic drag of blunt bodies at supersonic speeds. The aerospike creates a detached shock ahead of the body. Between the shock and the forebody a zone of recirculating flow occurs which acts like a more streamlined forebody profile, reducing ...
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 .
The United States Army intends to deploy the Long-Range Hypersonic Weapon in an eight missile battery containing four M983 trucks and trailers each holding two missiles in launch canisters alongside a command vehicle. [11] [12] The LRHW has been named Dark Eagle by the US Army. [36] [37] [38]
Traditional low nose cone designs (e.g. the McLaren MP4/4) allow the lower suspension arms to be directly attached to the main structural members of the car. However, since the move to high nose cone designs – which allow better use of airflow underneath the car, [ 2 ] and to a lesser extent the front wing – location of these lower arms has ...
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