Geometry Design of Coaxial Rigid Rotor in High-Speed Forward Flight

<div>Temporal variation of <svg height="11.8174pt" id="M57" style="vertical-align:-3.1815pt" version="1.1" viewbox="-0.0498162 -8.6359 15.1406 11.8174" width="15.1406pt" 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="M645 631C614 643 545 666 457 666C215 666 23 519 23 283C23 90 158 -16 337 -16C412 -16 489 2 522 10C543 39 590 127 606 167L580 181C519 89 459 18 348 18C201 18 122 136 122 287C122 464 244 632 435 632C544 632 602 595 608 472L639 475C643 526 645 581 645 631Z"></path></g><g transform="matrix(.0091,0,0,-0.0091,8.619,3.132)"><path d="M655 676H628C608 656 600 650 571 650H156C118 650 114 651 102 676H77C63 615 45 548 24 485L60 486C81 531 97 562 114 580C134 603 148 611 252 611H308L217 127C201 41 196 38 105 32L98 0H384L393 32C300 38 288 41 304 127L393 611H466C553 611 571 604 582 580C592 559 597 530 595 485L630 489C636 548 645 624 655 676Z"></path></g></svg> of the upper and lower rotors over one revolution.</div>

International Journal of Aerospace Engineering

Geometry Design of Coaxial Rigid Rotor in High-Speed Forward Flight

Figure 7