Experimental Study on Aerodynamic Heating Induced by Dual Injections into Hypersonic Cross Flow

<div>Schlieren photographs for the tandem dual injections at (a) <svg height="11.927pt" id="M74" style="vertical-align:-3.291101pt" version="1.1" viewbox="-0.0498162 -8.6359 48.5774 11.927" width="48.5774pt" 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="M449 634C442 637 425 643 405 650C376 660 341 666 307 666C181 666 98 590 98 485C98 400 170 343 215 310L246 288C307 243 343 204 343 147C343 67 291 18 219 18C104 18 61 124 51 202L23 199C28 124 27 71 27 47C47 22 122 -16 204 -16C324 -16 428 60 428 174C428 256 379 309 307 360L276 382C223 419 179 455 179 516C179 576 221 632 293 632C379 632 410 564 418 487L448 490C446 536 446 592 449 634Z" id="g113-84"></path><glyph.data ascent="3473" descent="-2876" horiz-adv-x="472" vert-adv-y="472"></glyph.data></g><g transform="matrix(.0091,0,0,-0.0091,6.071,3.132)"><path d="M545 403C545 425 527 451 498 451C448 451 400 404 312 286L290 341C262 412 246 451 219 451C182 451 138 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International Journal of Aerospace Engineering

fig11

Figure 11

Figure 11: Experimental Study on Aerodynamic Heating Induced by Dual Injections into Hypersonic Cross Flow 