747/747 GENERATOR /FOLLOWER CONFIGURATION AND ITS DYNAMICS RESPONSE

Flow Conditions

• Flow over a Boeing 747 wing is assumed fully turblent
• Reynolds Averaged Navier-Stokes Equations with Baldwin and Lomax turbulence model is used
• Reynolds Number is 1 million, angle of attack is zero degree and Mach Number is 0.3

Three flow cases are considered

Wing with vortex encounter at t = 0

Dynamic response of wing with vortex encounter at t=10
 

Dynamic response of wing with vortex encounter at t=20