Computation of Supersonic Flow over Flying Configurations

F

FADET I, 221, 279–283, 293, 355

FADET II, 221, 279, 282, 355

fictitious

potential, 59, 72

two-dimensional incompressible flow, 113

fields

pressure, 225

temperature, 225

velocity’s, 225

viscosity, 225

flap-surface, 273

flaps, 106, 109, 147, 157, 172, 173, 176, 177, 220

closed, 270

leading edge’s, 18, 172, 271, 354

in open (expanded) position, 147, 172, 270, 273, 295

in retracted (closed) position, 147, 172, 273

movable, 147, 157, 172, 270, 273, 355, 356

flat plate, 65, 207, 220

flattened FC, 4, 26, 34, 35–38, 58, 106, 189, 264, 271, 351

flattening, 286

flight

dynamics, 269, 285

mechanics, 185, 189, 221

navigation, 185, 189, 221

stability of, 221

supersonic, 351

with shock-free surfaces, 351

flow

chart, 283

computation of, 356

conical, 60