Sign in to FlowVella

Forgot password?
Sign in with Facebook

New? Create your account

Sign up for FlowVella

Sign up with Facebook

Already have an account? Sign in now


By registering you are agreeing to our
Terms of Service

Share This Flow

Loading Flow

loading...

Downloading Image /

loading...

Downloading Image /

loading...

Downloading Image /

loading...

Downloading Image /

loading...

Downloading Image /

loading...

Downloading Image /

loading...

Downloading Image /

loading...

Downloading Image /

loading...

Downloading Image /

loading...

Computational Fluid Dynamics

Sebastian

Analysed Lift/Drag and ratio shows the most effective wing planform.


Aerofoil data from CFD analysis :


- Reflex Camber : 25 %


- Thickness : 5 %


- Chord Length : 30 m


- Angle of Attack : 10°

Downloading Image /

loading...

Downloading Image /

loading...

Downloading Image /

loading...

Downloading Image /

loading...

Downloading Image /

loading...

Downloading Image /

loading...

Downloading Image /

loading...

Downloading Image /

loading...

Downloading Image /

loading...

Downloading Image /

loading...
  • 1

  • 2

  • 3

  • 4

  • 5

  • 6

  • 7

  • 8

  • 9

  • 10

  • 11

  • 12

  • 13

  • 14

  • 15

  • 16

  • 17

  • 18

  • 19

Ground Effect Vehicles - Presentation 3

By SebHDLawson