Index
Aerodynamic derivatives
body fixed/wind axes, 256, 267, 272, 280, 284, 432, 471, 485
flexible corrections, 238, 433, 439
inertial axes, 218, 231, 293, 471
oscillatory, 159
Aerodynamic Influence Coefficients (AICs), 194, 388–415, 433
harmonic motion, 394
modal space, 397
Aerodynamic(s), 69–85, 381–400
AICs – see Aerodynamic Influence Coefficients
Biot-Savart law, 391
centre of pressure, 74
centre, 76
CFD (Computational Fluid Dynamics), 432, 439
circulation, 386
Doublet Lattice method, 396, 409, 432
doublet, 383
drag, 74, 81, 213, 218, 267, 485
dynamic pressure, 72
horseshoe vortex, 392
Influence coefficients, 389
Kutta condition, 388
Mach No, 71
point sink/source, 382
quasi-steady, 153, 168, 173, 256, 295
Rankine oval, 384
Rational Fraction Approximation, 412, 434
stream function, 381
streamlines, 72
strip theory, 79, 212, 228, 236, 394, 432
supersonic flow – Piston theory, 83, 194
three D oscillating wing, 396
three D wing modelling, 77, 81, 391
transonic flows, 84
two D aerofoil modelling, 388
two D oscillating aerofoil, 394
unsteady, 154–165, 167, 187, 300, 313, 318, 325
velocity potential, 382
vortex filaments, 391
Vortex Lattice method, 393
vorticity, 386
Aeroelastic equations, 171, 402, 408
Aeroservoelasticity (ASE), see also, Flutter, 201–209, 441
closed loop system stability, 204
control law frequency dependence, 206
control ...
Get Introduction to Aircraft Aeroelasticity and Loads now with the O’Reilly learning platform.
O’Reilly members experience books, live events, courses curated by job role, and more from O’Reilly and nearly 200 top publishers.