Design and Simulation of Two Stroke Engines

More documents

Recommendations

Info

local acoustic velocity, 60 local Mach number, 60 mass flow rate, 60 particle velocity, 59 pressure amplitude ratio, 59 propagation velocity, 59 the expansion wave absolute pressure, 60 density, 60 local acoustic velocity, 60 local Mach number, 61 mass flow rate, 61-62 particle velocity, 61 pressure amplitude ratio, 61 propagation velocity, 61 shock formation (wave profile distortion) introduction, 62 compression waves (discussion), 62, 64 expansion waves (discussion), 63-64 flow diagram of, 63 particle velocity (shock wave), 62, 64 propagation velocity (shock wave), 62, 63 steep-fronting, 62 Pumping mean effective pressure determination of (in engine testing), 37-38 see also Friction/friction losses Purity charge purity CFD plots (Yamaha DT250 cylinders), 246-248 vs. crankshaft angle (chainsaw engine simulation), 386 in closed cycle combustion model (single-zone), 321 exhaust port purity correlated theoretical model (Yamaha DT250 cylinders), 239-240 theoretical calculation of, 238-239 theoretical curves (eight test cylinders), 239-240 idealized incoming scavenge flow, defined, 212 importance of (in Benson-Brandham model), 217-218 in mesh space J (during time step in GPB model), 161 scavenging purity, defined, 28 613 Index QUB (Queen's University of Belfast) air-assisted fuel injection system spray pattern, 519 Jante method, experience with, 222-223 laminar flow type silencer design, 565 QUB cross scavenging deflection ratio, importance of, 262 and homogeneous charge combustion, 338 piston design for (typical), 10, 11, 12 QUB CROSS ENGINE DRAW ((computer program)), 25-26 QUB CROSS PORTS ((computer program)), 260, 261-263 scavenging efficiency of, 11 squish action in, 262, 325, 338 SR vs. SE (QUBCR cylinder), 230 SR vs. TE (QUBCR cylinder), 231 QUB single-cycle scavenging test apparatus functional description, 224-227 see also Scavenging QUB SP single-pulse experimental apparatus introduction, 170 coefficient of discharge for, 172 convergent exhaust taper, 183-185 design criteria of, 171 divergent exhaust taper (long megaphone), 185-187 divergent exhaust taper (short), 181-183 effect of friction on outflow (straight pipe), 176 exhaust pipe with discontinuity, 188-191 functional description, 171-172 reference gas properties (CO2 and air, discontinuous exhaust), 188-189 straight pipe (inflow process), 175-177 straight pipe (outflow process), 173-175 sudden exhaust expansion, 177-179 QUB stratified charging engine air-fuel paths in (diagram), 498 bmep (at optimized fuel consumption levels), 499, 500 fuel consumption, optimized, 499 functional description, 498-499 QUB 250-cc racing-model engine, 1, 2 QUB 270 cross-scavenged airhead-stratified engine advantages of, 512 bmep vs. rpm, 510-511
Design and Simulation of Two-Stroke Engines QUB (Queen's University of Belfast) (continued) QUB 270 cross-scavenged airhead-stratified engine (continued) bsfc vs. rpm, 511 bsHCvs. rpm, 511-512 QUB 400 research engine AFR vs. oxygen emissions, 473, 475 bmep, AFR effect on, 472, 474, 476 bsCO, AFR effect on, 473-475 bsHC vs. air-fuel ratio, 473, 476 measured performance vs. AFR, 472-473 QUB LS400 SI engine combustion efficiency, 294, 296 heat release analysis, 294, 295 mass fraction burned, 294, 295 QUB 500rv research engine (various fueling) description and configuration, 522 multi-cylinder engine, basis for, 530 poppet valve timing, 523 test parameters (described), 523 stratified combustion in, 529-530 bmep vs. AFR (full load), 523 bmep vs. AFR (light load), 529 bsfc vs. AFR (full load), 524 bsfc vs. AFR (light load), 526 bsHC vs. AFR (full load), 524 bsHC vs. AFR (light load), 526 bsNOx vs. AFR (full load), 525 bsNOx vs. AFR (light load), 526, 527 Rankine-Hugoniot equations shock waves in unsteady gas flow, 75-77 Rassweiler, G.M. expression for incremental heat release (SI engines), 293 Reed valves introduction and discussion, 17 charging alternatives for, 17 design of, empirical carburetor flow diameter, determination of, 453 dummy reed block angle, use of, 455 empirical design, introduction to, 446-447 empirical design process, criteria for, 451 glass-fiber reed petals, durability of, 455 as pressure-loaded cantilevered beam, 453-454 614 reed block, rubber-coated (with steel reeds and stop plate), 447 reed flow area (Ar(j), determination of, 452 reed petal materials, 446, 451, 455 reed port area (Aq,), effective, 452 reed tip lift behavior, 448-450, 453 REED VALVE DESIGN computer program, 452, 454-455 stop-plate radius, determination of, 454 vibration and amplitude criteria, 453 see also Specific time area (Asv) design of, general design dimensions (reed petal, reed block), 367 as pressure-loaded cantilevered beam, 368-369 in racing motorcycle engine simulation, 394, 401-402 reed block, flow restrictions from, 369 reed block, placement and function of, 368 reed flow area (Arcj), determination of, 369 reed port area (A^,), effective, 369 reed tip lift ratio, 370 in Grand Prix motorcycle racing engine, 17,19 reed vs. disc valves (discussion), 446-447 typical configurations, 16, 367 Reid, M.G.O. mass fraction burned experimental data (SI engine), 310-312 Reimann variables in simulation of engines (using unsteady gas flow), 142, 143 research funding, comment on, 192 Reynolds number in crankcase heat transfer analysis, 376 and heat release analysis (SI engines), 305-306 in heat release analysis (SI engines), 305-306 in pressure wave propagation friction factor (straight pipes), 82 in scavenging flow (experimental assessment of), 223 Ricardo Comet (IDI diesel engine) combustion chamber geometry, 317 Rich limit (for diesel combustion), 288 Rich mixture combustion, 288, 299-300 Rootes-Tilling-Stevens diesel road engines, 3
Page 2 and 3:
Design and Simulation of Two-Stroke
Page 4 and 5:
A Second Mulled Toast When as a stu
Page 6 and 7:
Page 8 and 9:
Acknowledgments As explained in the
Page 10 and 11:
Table of Contents Nomenclature xv C
Page 12 and 13:
Table of Contents 2.10.1 Flow at pi
Page 14 and 15:
Table of Contents 3.5.3.1 The use o
Page 16 and 17:
Table of Contents 6.1.3 The effect
Page 18 and 19:
Nomenclature NAME SYMBOL UNIT (SI)
Page 20 and 21:
speed of rotation speed of rotation
Page 22 and 23:
attenuation or transmission loss wa
Page 24 and 25:
Page 26 and 27:
Page 28 and 29:
Page 30 and 31:
Page 32 and 33:
Page 34 and 35:
Page 36 and 37:
Page 38 and 39:
Page 40 and 41:
Page 42 and 43:
Page 44 and 45:
Page 46 and 47:
Page 48 and 49:
Page 50 and 51:
Page 52 and 53:
Page 54 and 55:
Page 56 and 57:
Page 58 and 59:
Page 60 and 61:
Page 62 and 63:
Page 64 and 65:
Page 66 and 67:
Page 68 and 69:
Page 70 and 71:
Page 72 and 73:
Page 74 and 75:
Page 76 and 77:
Page 78 and 79:
Page 80 and 81:
Page 82 and 83:
Page 84 and 85:
Page 86 and 87:
Page 88 and 89:
Page 90 and 91:
Page 92 and 93:
Page 94 and 95:
Page 96 and 97:
Page 98 and 99:
Page 100 and 101:
Page 102 and 103:
Page 104 and 105:
Page 106 and 107:
Page 108 and 109:
Page 110 and 111:
Page 112 and 113:
Page 114 and 115:
Page 116 and 117:
Page 118 and 119:
Page 120 and 121:
Page 122 and 123:
Page 124 and 125:
Page 126 and 127:
Page 128 and 129:
Page 130 and 131:
Page 132 and 133:
Page 134 and 135:
Page 136 and 137:
Page 138 and 139:
Page 140 and 141:
Page 142 and 143:
Page 144 and 145:
Page 146 and 147:
Page 148 and 149:
Page 150 and 151:
Page 152 and 153:
Page 154 and 155:
Page 156 and 157:
Page 158 and 159:
Page 160 and 161:
Page 162 and 163:
Page 164 and 165:
Page 166 and 167:
Page 168 and 169:
Page 170 and 171:
Page 172 and 173:
Page 174 and 175:
Page 176 and 177:
Page 178 and 179:
Page 180 and 181:
Page 182 and 183:
Page 184 and 185:
Page 186 and 187:
Page 188 and 189:
Page 190 and 191:
Page 192 and 193:
Page 194 and 195:
Page 196 and 197:
Page 198 and 199:
Page 200 and 201:
Page 202 and 203:
Page 204 and 205:
Page 206 and 207:
Page 208 and 209:
Page 210 and 211:
Page 212 and 213:
Page 214 and 215:
Page 216 and 217:
Page 218 and 219:
Page 220 and 221:
Design and Simulation ofTwo-Stroke
Page 222 and 223:
Page 224 and 225:
Page 226 and 227:
Page 228 and 229:
Page 230 and 231:
Page 232 and 233:
Page 234 and 235:
Page 236 and 237:
Page 238 and 239:
Page 240 and 241:
Page 242 and 243:
Page 244 and 245:
Page 246 and 247:
Page 248 and 249:
Page 250 and 251:
Page 252 and 253:
Page 254 and 255:
Page 256 and 257:
Page 258 and 259:
Page 260 and 261:
Page 262 and 263:
Page 264 and 265:
Page 266 and 267:
Page 268 and 269:
Design and Simulation ofTwo'Stroke
Page 270 and 271:
Page 272 and 273:
Page 274 and 275:
Page 276 and 277:
Page 278 and 279:
Page 280 and 281:
Page 282 and 283:
Page 284 and 285:
Page 286 and 287:
Page 288 and 289:
Page 290 and 291:
Page 292 and 293:
Page 294 and 295:
Page 296 and 297:
Page 298 and 299:
Page 300 and 301:
Page 302 and 303:
Chapter 4 Combustion in Two-Stroke
Page 304 and 305:
Chapter 4 - Combustion in Two-Strok
Page 306 and 307:
Page 308 and 309:
Page 310 and 311:
a stratilpl o tions to ivior. If m
Page 312 and 313:
Page 314 and 315:
Page 316 and 317:
CD 30 -, W 20 - LU CO iS _J LU OC 1
Page 318 and 319:
Page 320 and 321:
Page 322 and 323:
181 also x3 = — = 0.905 x6 = 2.17
Page 324 and 325:
to be cur .3.20) .3.21) .3.22) for
Page 326 and 327:
3.23) com- :on is hhas has a /eng-
Page 328 and 329:
stroke .3.29) mean me to 3land ssio
Page 330 and 331:
Page 332 and 333:
a LU z: en 3 CO a LU z EC D m O ho
Page 334 and 335:
CD 1.2 -i 1.0 - di „„ LU 0.8 cc
Page 336 and 337:
CO —> 111" cc LU < LU _J LU CC £
Page 338 and 339:
Page 340 and 341:
Page 342 and 343:
Combustion in compression-ignition
Page 344 and 345:
Page 346 and 347:
Page 348 and 349:
stroke ari more often lseful lental
Page 350 and 351:
lat the ssi ;tribu- ELEVATION VIEWS
Page 352 and 353:
CYLINDER HEAD TYPE IS CENTRAL BORE,
Page 354 and 355:
Page 356 and 357:
CO E 50 40 - O O _i Hi > I CO 30 Z)
Page 358 and 359:
CURRENT INPUT DATA FOR 2-STROKE 'SP
Page 360 and 361:
Page 362 and 363:
Cylin- PP £ Pa- tics of Paper Chap
Page 364 and 365:
vfitro- ;titi >tants 1970. i(In- Ch
Page 366 and 367:
Page 368 and 369:
Page 370 and 371:
£2 = Pi P2 I Pi J Chapter 4 - Comb
Page 372 and 373:
CHAINSAW AT 9600 rpm. Chapter 4- Co
Page 374 and 375:
LLI •z. O N -z. 0.21 -, 0.20 DC 0
Page 376 and 377:
Page 378 and 379:
Page 380 and 381:
Page 382 and 383:
Page 384 and 385:
Page 386 and 387:
Page 388 and 389:
Page 390 and 391:
Page 392 and 393:
Page 394 and 395:
Page 396 and 397:
Page 398 and 399:
Page 400 and 401:
Page 402 and 403:
Page 404 and 405:
Page 406 and 407:
Page 408 and 409:
Page 410 and 411:
Page 412 and 413:
Page 414 and 415:
Page 416 and 417:
Page 418 and 419:
Page 420 and 421:
Page 422 and 423:
Page 424 and 425:
Page 426 and 427:
Page 428 and 429:
Page 430 and 431:
Page 432 and 433:
Page 434 and 435:
Page 436 and 437:
Page 438 and 439:
Page 440 and 441:
Page 442 and 443:
Page 444 and 445:
Page 446 and 447:
Page 448 and 449:
Page 450 and 451:
Page 452 and 453:
Page 454 and 455:
Page 456 and 457:
Page 458 and 459:
Page 460 and 461:
Page 462 and 463:
Page 464 and 465:
Page 466 and 467:
Page 468 and 469:
Page 470 and 471:
Page 472 and 473:
Page 474 and 475:
Page 476 and 477:
Page 478 and 479:
Page 480 and 481:
Page 482 and 483:
Chapter 7 Reduction of Fuel Consump
Page 484 and 485:
Chapter 7 • Reduction of Fuel Con
Page 486 and 487:
Chapter 7 - Reduction of Fuel Consu
Page 488 and 489:
Page 490 and 491:
Page 492 and 493:
^ s C£ Q 2^ E Q. Q_ z' o ISSI HCEM
Page 494 and 495:
o > z~ Q w CO UJ w g x O z o z o m
Page 496 and 497:
S.S.F.C. , C./SHP-HS Chapter 7 - Re
Page 498 and 499:
Page 500 and 501:
Page 502 and 503:
Page 504 and 505:
Page 506 and 507:
Page 508 and 509:
0.35 • 0.34 LU ° 0.33 - c 03 DC
Page 510 and 511:
Page 512 and 513:
§ 2000
Page 514 and 515:
y, ,6 Chapter 7 - Reduction of Fuel
Page 516 and 517:
Page 518 and 519:
Page 520 and 521:
Chapter 7- Reduction of Fuel Consum
Page 522 and 523:
Page 524 and 525:
INLET FOR r AIR AND FUEL Chapter 7
Page 526 and 527:
Page 528 and 529:
o Q_ Ld < CD 15-, 10- Chapter 7 - R
Page 530 and 531:
6. £ -Q 500 n | "I) 400 -Q 300 100
Page 532 and 533:
Page 534 and 535:
Page 536 and 537:
Page 538 and 539:
Page 540 and 541:
Page 542 and 543:
Page 544 and 545:
JZ x" O Z CO J3 20 i 10 - 10 Chapte
Page 546 and 547:
$ 2 - x O z 2 1 Chapter 7 - Reducti
Page 548 and 549:
Page 550 and 551:
Page 552 and 553:
Page 554 and 555:
Page 556 and 557:
Page 558 and 559:
O 01 III cr cc LU Q. LU h- LU Z o N
Page 560 and 561:
Chapter 8 Reduction of Noise Emissi
Page 562 and 563:
Chapter 8 • Reduction of Noise Em
Page 564 and 565:
Chapter 8 - Reduction of Noise Emis
Page 566 and 567:
Page 568 and 569:
Page 570 and 571:
1 28.6 ^ i d>2£ 1.6 \ f > < 4)28.6
Page 572 and 573:
Page 574 and 575:
Page 576 and 577:
Page 578 and 579:
Page 580 and 581: Chapter 8 - Reduction of Noise Emis
Page 592 and 593: Chapter 8 • Reduction of Noise Em
Page 596 and 597: H Chapter 8 - Reduction of Noise Em
Page 598 and 599: Name F R Chapter 8 • Reduction of
Page 602 and 603: 1 Chapter 8 - Reduction of Noise Em
Page 606 and 607: • • / . • Appendix Listing of
Page 608 and 609: Active radical (AR) combustion and
Page 610 and 611: initial conditions, assumptions reg
Page 612 and 613: in two-stroke engine (schematic dia
Page 614 and 615: exhaust timing control valve, effec
Page 616 and 617: I Exhaust emissions/exhaust gas ana
Page 618 and 619: Exhaust systems (continued) untuned
Page 620 and 621: gas constant/universal gas constant
Page 622 and 623: in crankcase heat transfer analysis
Page 624 and 625: Mercury Marine air-assisted fuel in
Page 626 and 627: I PISTON POSITION (computer program
Page 628 and 629: Pressure wave reflection (in pipes)
Page 632 and 633: Roots blower in turbocharged/superc
Page 634 and 635: Scavenging (continued) scavenging e
Page 636 and 637: Simulation, engine See Computer mod
Page 638 and 639: temperature vs. crankshaft angle (c
Page 640 and 641: work per thermodynamic (Otto) cycle
show all

Design and Simulation of Two Stroke Engines

Create successful ePaper yourself

Delete template?

Save as template?