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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.
File:Elliptical Nose Cone Render.png. Add languages. ... (1,002 × 882 pixels, file size: 257 KB, MIME type: image/png) This is a file from the Wikimedia Commons.
English: Render from SolidWorks CAD program of a bi-conic-shaped rocket nose cone with a total length of 18 inches, a primary radius of 4 inches, a secondary (tip) section length of 6 inches, and a secondary radius of 2 inches.
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.
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 .
1. Sign in to your AOL account. 2. Click your profile name. 3. Click Personal Info. 4. Click Update profile photo. 5. Select Upload from device. 6. Edit the photo by cropping or rotating it, or by adding a filter.
This image might not be in the public domain outside of the United States; this especially applies in the countries and areas that do not apply the rule of the shorter term for US works, such as Canada, Mainland China (not Hong Kong or Macao), Germany, Mexico, and Switzerland. The creator and year of publication are essential information and ...
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.