Computation of Supersonic Flow over Flying Configurations

P

parabola, 248

black, 248, 253

critical, 247, 248–251

peak of, 247, 248

parabolic dependence, 207, 220

parallel

flow, 38, 91, 161, 271, 354

parameters

of optimization, 272, 274, 276, 278, 330

of similarity, 40, 45, 49, 53, 56, 79, 114, 157, 161, 171, 191, 270, 272, 276, 316, 330, 350

partial derivatives

of first order, 2, 4, 5, 107, 108

of second order, 4, 5, 28, 32

of nth order, 107, 110, 111

partial differential equations (PDEs), 1, 2, 12, 26, 28, 30, 56, 225, 256, 354, 356

of NSL, 1–19, 225, 252, 256

of absolute temperature, 3, 16–17

of continuity, 2, 10, 21–23

of energy, 3, 21, 23

of impulse, 12–13, 21, 25

of internal energy, 3, 23

of temperature, 3

linear PDEs, 26–28

of first order in R, 18

PDEs of second order (quadratic type), 225