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Ouissem B.
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Paris, France
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Lockheed Martin Blended Wing-Body
AoA = 2.4 Mach = 0.72 Altitude = 10000 m
4
53
4
NASA Supersonic Bizjet
AoA = 0.0 Mach = 2.0 Altitude = 12000 m RANS Computation
5
9
0
NASA N2A Hybrid Wing Body
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...
3
36
3
Boeing 787-300
Boeing 787-300 Euler Computation AoA = 0.0 Mach = 0.78
1
17
0
Future Transport Aircraft
Future Transport Aircraft w/ variable winglets toe. Design by J. Philip Barnes Euler computation AoA = 0.0 Mach = 0.78
1
12
0
Embraer ATR 42-600
Euler computation AoA = 0.0 Mach = 0.7
7
32
1
Free-model Racing Car
RANS simulation Cp on the surface of a racing car. U ~ 348 km/h. CDrag: 0.45 CLift: -0.12
2
13
1
High-Speed Civil Transport Aircraft
The 'High-Speed Civil Transport' Aircraft is a supersonic civil aircraft developed by Boeing Commercial Airplanes and NASA Langley Research Center ...
7
12
0
Honda HA-420 HondaJet
Compressible RANS simulation Mach = 0;72 Altitude = 12500 m Photo 1: Pressure coefficient on the aircraft surface. Photo 2: CFD surface mesh.
2
48
1
Free-model Car
Compressible RANS simulation Photo 1: Freestream velocity of 90 km/h. Photo 2: Speed of 240 km/h. Max speed of 312 km/h. Free-model geometr...
6
29
1
