Computation of Supersonic Flow over Flying Configurations

Subject Index

A

absolute temperature, 1–2, 9, 11, 16, 23, 252, 257

partial differential equation (PDE) of, 2

acceleration, 153

of convergence, 153

accurate, 18, 266

adaptor, 296, 343

interchangeable, 297

aerodynamics, 156

high speed

theoretical, 186

aerodynamical

applications, 18, 252, 264, 266

fully-optimized, 26, 285–286, 293, 295, 296, 297, 327

global, 270, 271, 273, 277

inviscid, 270, 273, 277

iterative, 273, 283

viscous, 18, 153, 283

load, 185, 189, 221

optimal design, 18, 57, 172, 225, 256, 283, 355

of shape, 18, 56, 57, 172, 182

optimum-optimorum design, 185, 225, 256, 270, 271–273, 283–285

performance, 256, 269, 327, 356

aerodynamical characteristics, 33, 59, 65, 95, 152, 158, 165–172, 180, 181, 182, 183, 185, 215, 220, 221, 292