Gust Response Analysis for Helicopter Rotors in the Hover and Forward Flights

<div>Angle of attack at the tip element due to <svg height="8.69875pt" id="M184" style="vertical-align:-0.3499298pt" version="1.1" viewbox="-0.0498162 -8.34882 36.797 8.69875" width="36.797pt" xmlns="http://www.w3.org/2000/svg" xmlns:xlink="http://www.w3.org/1999/xlink"><g transform="matrix(.013,0,0,-0.013,0,0)"><path d="M384 0V27C293 34 287 42 287 114V635C232 613 172 594 109 583V559L157 557C201 555 205 550 205 499V114C205 42 199 34 109 27V0H384Z" id="g113-50"></path><glyph.data ascent="3473" descent="-2876" horiz-adv-x="480" vert-adv-y="480" xpluscharwidth="6.24"></glyph.data></g><g transform="matrix(.013,0,0,-0.013,9.145,0)"><path d="M535 230V280H52V230H535Z" id="g117-33"></path><glyph.data ascent="3473" descent="-2876" horiz-adv-x="587" vert-adv-y="587" xpluscharwidth="16.776"></glyph.data></g><g transform="matrix(.013,0,0,-0.013,19.682,0)"><path d="M390 111C344 68 312 56 269 56C212 56 118 102 118 241C118 346 175 401 241 401C277 401 312 388 342 360C350 352 355 349 361 349C372 349 394 371 394 392C394 403 391 411 378 422C362 436 329 449 288 449H287C250 449 190 432 138 392C71 341 37 274 37 197C37 90 112 -12 238 -12C297 -12 363 32 407 90L390 111Z" id="g121-97"></path><glyph.data ascent="989" descent="-360" horiz-adv-x="423" vert-adv-y="423" xpluscharwidth="25.180999999999997"></glyph.data></g><g transform="matrix(.013,0,0,-0.013,25.181,0)"><path d="M257 449C165 449 37 374 37 209C37 98 119 -12 256 -12C355 -12 473 65 473 226C473 349 381 449 257 449ZM244 416C333 416 380 320 380 204C380 67 329 21 267 21C184 21 130 115 130 241C130 354 184 416 244 416Z" id="g121-109"></path><glyph.data ascent="989" descent="-360" horiz-adv-x="510" vert-adv-y="510" xpluscharwidth="31.811"></glyph.data></g><g transform="matrix(.013,0,0,-0.013,31.811,0)"><path d="M319 325C317 349 306 409 297 431C277 440 250 449 209 449C117 449 57 389 57 319C57 243 122 209 182 182C232 159 261 135 261 91C261 48 227 21 190 21C130 21 85 79 68 145L41 140C41 104 51 36 58 22C75 7 121 -12 172 -12C252 -12 337 35 337 126C337 195 286 231 210 262C166 281 126 304 126 348C126 388 152 417 191 417C240 417 274 378 294 318L319 325Z" id="g121-113"></path><glyph.data ascent="989" descent="-360" horiz-adv-x="367" vert-adv-y="367" xpluscharwidth="36.582"></glyph.data></g></svg> gust at the advanced ratio of 0.2.</div>

Shock and Vibration

fig22

Figure 22

Figure 22: Gust Response Analysis for Helicopter Rotors in the Hover and Forward Flights 