SPICES-2009

 

Geometric Details:

  1 .  Mean Aerodynamic Chord (MAC)  =   1.00584 m.
  2 .  Reference Span                               =   2.16154 m.
  3 .  Half Model Reference Area (S)      =  2.046468165 m2.
  

Test Conditions: 

  1 .  Mach Number           =  0.2.
  2 .  Reynolds Number      =  4.3 million.


Grids

Unstructured Grid for the NASA Trap Wing Configurations used in the SPICES-2009 workshop can be downloaded from the following link.

README

UG1:

TrapWing_UG1.cgns.gz
TrapWing_UG1.msh.gz

UG2:

TrapWing_UG2.cgns.gz
TrapWing_UG2.msh.gz

 

 

Summary Report of SPICES-2009 can be downloaded from the link given below.

Download Report