International Journal of Aerospace Engineering / 2016 / Article / Tab 2

Research Article

Aeroelastic Analysis of Wings in the Transonic Regime: Planform’s Influence on the Dynamic Instability

Table 2

CFD boundary conditions.

Swept wing modelCurved wing model

Altitudes analysed0 m–10000 m0 m–10000 m
Pressure far fieldFront side up downFront side up down
Pressure outletRearRear
SymmetryCenter-line planeCenter-line plane
Wall/no slipWing surfaceWing surface