Another CFD result showing the MDXX and how the shock vanishes close to the fuselage where the aerofoil is more slender
NASA AD-1,==Glej tudi==*Letalsko krilo*Različne konfiguracije kril*Delta krilo*Kantilever krilo*Krilo z negativnim naklonom*Gibljivo krilo*Krilo s spremenljivim geometrijskim kotom==Sklici in reference====Bibliografija====Zunanje povezave==*"Swept Wings and Effective Dihedral"*The development of swept wings*Simple sweep theory math*Advanced math of swept and oblique wings*The L-39 and swept wing research*Sweep theory in a 3D environment*CFD results showing the three-dimensional supersonic bubble over the wing of an A 320.