A numerical method based on the vortex methodology is presented in order to obtain unsteady solution of the aerodynamic coefficients of a thin airfoil in either compressible ... (Soviero and Ribeiro, ...

Stage one FTS is saved. Stage one entry burn shut down. Stage 2 FTS is saved. Stage one Transonic. Stage one landing burn. Stage 2 terminal guidance. Stage one landing like deploy. Stage one ...