Principles of Helicopter AerodynamicsHelicopters are highly capable and useful rotating-wing aircraft with roles that encompass a variety of civilian and military applications. Their usefulness lies in their unique ability to take off and land vertically, to hover stationary relative to the ground, and to fly forward, backward, or sideways. These unique flying qualities, however, come at a high cost including complex aerodynamic problems, significant vibrations, high levels of noise, and relatively large power requirements compared to fixed-wing aircraft. This book, written by an internationally recognized expert, provides a thorough, modern treatment of the aerodynamic principles of helicopters and other rotating-wing vertical lift aircraft. Every chapter is extensively illustrated and concludes with a bibliography and homework problems. Advanced undergraduate and graduate students, practising engineers, and researchers will welcome this thorough and up-to-date text on rotating-wing aerodynamics. |
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Contents
VI | 1 |
VII | 2 |
VIII | 12 |
IX | 14 |
X | 22 |
XII | 27 |
XIII | 28 |
XIV | 29 |
CXLIV | 225 |
CXLV | 226 |
CXLVII | 227 |
CXLVIII | 229 |
CXLIX | 232 |
CLI | 233 |
CLII | 234 |
CLIII | 235 |
XV | 30 |
XVI | 33 |
XVII | 36 |
XVIII | 37 |
XIX | 38 |
XX | 39 |
XXI | 42 |
XXII | 43 |
XXIV | 44 |
XXV | 46 |
XXVI | 47 |
XXVII | 48 |
XXVIII | 50 |
XXIX | 52 |
XXX | 53 |
XXXII | 55 |
XXXIII | 57 |
XXXIV | 59 |
XXXV | 60 |
XXXVII | 63 |
XXXVIII | 64 |
XXXIX | 65 |
XL | 66 |
XLI | 67 |
XLII | 68 |
XLIII | 69 |
XLIV | 73 |
XLVI | 76 |
XLVII | 78 |
XLVIII | 80 |
XLIX | 82 |
LI | 83 |
LII | 84 |
LIV | 85 |
LV | 87 |
LVI | 91 |
LVII | 92 |
LVIII | 93 |
LIX | 96 |
LX | 99 |
LXI | 100 |
LXII | 102 |
LXIII | 105 |
LXIV | 106 |
LXV | 107 |
LXVI | 110 |
LXVIII | 111 |
LXX | 112 |
LXXII | 113 |
LXXIV | 114 |
LXXV | 115 |
LXXVI | 123 |
LXXVII | 124 |
LXXVIII | 126 |
LXXIX | 128 |
LXXX | 129 |
LXXXI | 131 |
LXXXII | 133 |
LXXXIII | 134 |
LXXXIV | 139 |
LXXXVII | 140 |
LXXXVIII | 141 |
LXXXIX | 142 |
XC | 144 |
XCI | 147 |
XCII | 149 |
XCIII | 150 |
XCIV | 155 |
XCV | 156 |
XCVI | 157 |
XCVII | 159 |
XCVIII | 163 |
C | 164 |
CII | 166 |
CV | 167 |
CVI | 168 |
CVII | 169 |
CIX | 170 |
CX | 171 |
CXI | 173 |
CXII | 174 |
CXIV | 176 |
CXV | 178 |
CXVI | 180 |
CXVII | 182 |
CXVIII | 184 |
CXIX | 185 |
CXX | 189 |
CXXI | 190 |
CXXII | 191 |
CXXIII | 193 |
CXXIV | 194 |
CXXV | 195 |
CXXVI | 197 |
CXXVII | 199 |
CXXVIII | 201 |
CXXIX | 203 |
CXXX | 204 |
CXXXI | 208 |
CXXXII | 209 |
CXXXIII | 212 |
CXXXIV | 213 |
CXXXV | 218 |
CXXXVI | 219 |
CXXXVIII | 220 |
CXXXIX | 222 |
CXLII | 223 |
CXLIII | 224 |
CLIV | 236 |
CLV | 237 |
CLVI | 243 |
CLVII | 244 |
CLVIII | 245 |
CLIX | 246 |
CLX | 247 |
CLXI | 251 |
CLXII | 253 |
CLXIII | 256 |
CLXIV | 257 |
CLXV | 258 |
CLXVI | 260 |
CLXVIII | 262 |
CLXIX | 264 |
CLXXI | 267 |
CLXXII | 268 |
CLXXIII | 269 |
CLXXIV | 272 |
CLXXV | 274 |
CLXXVI | 276 |
CLXXVII | 279 |
CLXXVIII | 285 |
CLXXIX | 288 |
CLXXXI | 289 |
CLXXXIII | 290 |
CLXXXIV | 291 |
CLXXXV | 293 |
CLXXXVI | 295 |
CLXXXVII | 296 |
CLXXXVIII | 298 |
CLXXXIX | 302 |
CXC | 303 |
CXCII | 306 |
CXCIII | 307 |
CXCIV | 308 |
CXCV | 309 |
CXCVI | 313 |
CXCVII | 315 |
CXCIX | 318 |
CC | 322 |
CCII | 323 |
CCIII | 326 |
CCIV | 328 |
CCV | 333 |
CCVI | 336 |
CCVII | 337 |
CCVIII | 340 |
CCIX | 342 |
CCX | 345 |
CCXI | 346 |
CCXII | 348 |
CCXIII | 349 |
CCXIV | 351 |
CCXVI | 353 |
CCXVII | 355 |
CCXVIII | 357 |
CCXIX | 358 |
CCXX | 359 |
CCXXI | 361 |
CCXXII | 363 |
CCXXIII | 365 |
CCXXIV | 367 |
CCXXV | 369 |
CCXXVI | 371 |
CCXXVII | 372 |
CCXXVIII | 374 |
CCXXIX | 378 |
CCXXX | 379 |
CCXXXI | 382 |
CCXXXIII | 383 |
CCXXXIV | 389 |
CCXXXV | 390 |
CCXXXVI | 393 |
CCXXXVII | 397 |
CCXXXVIII | 399 |
CCXXXIX | 403 |
CCXL | 405 |
CCXLI | 410 |
CCXLIII | 412 |
CCXLIV | 413 |
414 | |
CCXLVI | 418 |
CCXLVII | 419 |
CCXLIX | 421 |
CCLI | 425 |
CCLII | 426 |
CCLIII | 427 |
CCLIV | 431 |
CCLVII | 432 |
CCLVIII | 434 |
CCLIX | 435 |
CCLX | 440 |
CCLXI | 442 |
CCLXII | 443 |
CCLXIII | 445 |
CCLXIV | 446 |
CCLXV | 448 |
CCLXVI | 450 |
CCLXVII | 453 |
CCLXVIII | 458 |
CCLXIX | 470 |
CCLXX | 476 |
CCLXXI | 477 |
CCLXXII | 479 |
CCLXXIII | 487 |
489 | |
Other editions - View all
Common terms and phrases
advance aerodynamic aircraft airfoil airloads analysis angle of attack approach approximation assumed becomes blade boundary Chapter characteristics chord climb coefficient compared computational considered constant convection Data source disk distribution drag dynamic stall edge effects equation example experimental experiments factor Figure flapping flow force forward flight frequency function fuselage given gives gust helicopter rotor higher hinge hover increasing indicial induced induced velocity inflow lateral leading lift coefficient lift force linear loading lower Mach number main rotor maximum means measurements methods momentum NACA normal Note obtained operating performance pitch position power required predictions pressure problem produced ratio reduced relatively Representative response rotor disk rotor wake separation shown in Fig shows solidity solution speed surface tail rotor theory thrust tip vortex twist unsteady values variation various vertical vortex weight
Popular passages
Page 485 - Computation of Helicopter Rotor Wake Geometry and Its Influence on Rotor Harmonic Airloads," MIT Aeroelastic and Structures Research Laboratory Report (to be published).