NASA N2A Hybrid Wing Body 3d model
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NASA N2A Hybrid Wing Body

NASA N2A Hybrid Wing Body

by GrabCAD
Last crawled date: 1 year, 12 months ago
CFD Analysis of NASA N2A Hybrid Wing Body

Euler Computation

Fig. 1: Shock Pattern. Flow at Speed of Mach 2.4*
Fig. 2: 3D View. Mach 0.8 at a 20000 Ft. altitude

*The N2A Hybrid Wing is not designed to fly at Mach 2.4. It's cruising speed is Mach 0.8 at 35000 Ft. altitude.

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