stlfinder - 3d models search engine stlfinder - 3d models search engine
NASA N2A Hybrid Wing Body

NASA N2A Hybrid Wing Body

grabcad

In this CFD analysis of NASA's N2A Hybrid Wing Body, Euler computation was used. Figure 1 illustrates the shock pattern at a supersonic speed of Mach 2.4, while Figure 2 presents a 3D view of the flow at subsonic Mach 0.8 and an altitude of 20,000 feet. Note that the N2A Hybrid Wing is not designed for Mach 2.4; its cruising speed is Mach 0.8 at a higher altitude of 35,000 feet.

Download Model from grabcad

With this file you will be able to print NASA N2A Hybrid Wing Body with your 3D printer. Click on the button and save the file on your computer to work, edit or customize your design. You can also find more 3D designs for printers on NASA N2A Hybrid Wing Body.