A Preliminary Research on Combustion Characteristics of a Novel-Type Scramjet Combustor

<div>The density distribution of different surface parallel to the <svg height="8.80315pt" id="M76" style="vertical-align:-0.04981041pt" version="1.1" viewbox="-0.0498162 -8.75334 16.5019 8.80315" width="16.5019pt" 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="M655 0V28C585 35 563 50 517 120C469 193 414 280 360 366C427 469 460 516 481 545C526 604 545 614 619 622V650H391V622C457 614 462 604 438 560C411 511 381 463 339 398C295 466 258 523 225 580C210 606 211 615 272 622V650H26V622C98 614 111 603 154 538C189 482 235 408 288 324C200 188 149 116 124 85C95 47 64 34 7 28V0H236V28C169 36 164 46 188 89C220 148 261 217 310 291C372 193 417 118 442 77C461 44 454 35 392 28V0H655Z"></path></g><g transform="matrix(.013,0,0,-0.013,8.502,0)"><path d="M561 176C543 127 527 95 506 73C478 43 441 36 316 36C247 36 185 38 153 42C290 245 427 439 566 636L559 650H160C130 650 119 652 107 675H83C81 630 76 555 71 492L100 491C112 535 123 560 135 578C152 605 168 614 276 614H449C310 411 169 213 29 15L37 0H554C565 41 583 134 590 170L561 176Z"></path></g></svg> plane.</div>

International Journal of Aerospace Engineering

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Figure 10

Figure 10: A Preliminary Research on Combustion Characteristics of a Novel-Type Scramjet Combustor 