Index
A, B
acoustic impedance, 569
adapted nozzle, 248
adapted supersonic air intake, 418
adiabatic
process, 46
wall, 108
aerodynamic
balance, 125
moment, 1
resultant, 8
torsor, 32
aeroelastic coupling, 20
buzz, 658
area-Mach number relation, 216
attached shock, 342
Avogadro number, 82
axial force, 9
coefficient, 11
B
barotropic, 181
Bernoulli relation, 226
Betz method, 125
blow-down wind tunnels, 107
Boltzmann
constant, 82
equation, 85
boundary
conditions, 571
layer bleed system, 426
Bréguet’s formula, 15
buffeting, 658
bulk or volume viscosity, 95
Busemann pressure number, 447
C
calculable domains, 631
calorically perfect, 51
captation drag, 118
Carrière development method, 487
case of the over-expanded jet, 528
centered expansion, 455
wave, 559
centered Prandtl-Meyer expansion, 454
CFL criterion (Courant–Friedrich–Lewy), 642
characteristic
curve, 442
directions, 544
dissociation of temperature, 67
equations, 444
ionization temperature, 70
relations, 446
mesh, 504
chemical relaxation, 123
compressibility
correction, 663
factor, 54
compression wave, 460, 561, 645
condition of adherence, 107
conical
nozzles, 232
shock wave, 368
conicity factor, 242
contact surface, 584
continuity equation, 85
continuous
flow, 82
regime, 81
contoured (or ideal) nozzles, 232
conventional thrust, 242
at the pressure, 243
convergent-divergent supersonic nozzle, 215
corrector step, 641 ...
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