Neil McCartney - Properties for Design of Composite Structures

Здесь есть возможность читать онлайн «Neil McCartney - Properties for Design of Composite Structures» — ознакомительный отрывок электронной книги совершенно бесплатно, а после прочтения отрывка купить полную версию. В некоторых случаях можно слушать аудио, скачать через торрент в формате fb2 и присутствует краткое содержание. Жанр: unrecognised, на английском языке. Описание произведения, (предисловие) а так же отзывы посетителей доступны на портале библиотеки ЛибКат.

Properties for Design of Composite Structures: краткое содержание, описание и аннотация

Предлагаем к чтению аннотацию, описание, краткое содержание или предисловие (зависит от того, что написал сам автор книги «Properties for Design of Composite Structures»). Если вы не нашли необходимую информацию о книге — напишите в комментариях, мы постараемся отыскать её.

PROPERTIES FOR DESIGN OF COMPOSITE STRUCTURES
A comprehensive guide to analytical methods and source code to predict the behavior of undamaged and damaged composite materials Properties for Design of Composite Structures: Theory and Implementation Using Software
Properties for Design of Composite Structures: Theory and Implementation Using Software

Properties for Design of Composite Structures — читать онлайн ознакомительный отрывок

Ниже представлен текст книги, разбитый по страницам. Система сохранения места последней прочитанной страницы, позволяет с удобством читать онлайн бесплатно книгу «Properties for Design of Composite Structures», без необходимости каждый раз заново искать на чём Вы остановились. Поставьте закладку, и сможете в любой момент перейти на страницу, на которой закончили чтение.

Тёмная тема
Сбросить

Интервал:

Закладка:

Сделать

276 266

277 267

278 268

279 269

280 270

281 271

282 272

283 273

284 274

285 275

286 276

287 277

288 278

289 279

290 280

291 281

292 282

293 283

294 284

295 285

296 286

297 287

298 288

299 289

300 290

301 291

302 292

303 293

304 294

305 295

306 296

307 297

308 298

309 299

310 300

311 301

312 302

313 303

314 304

315 305

316 306

317 307

318 308

319 309

320 310

321 311

322 312

323 313

324 314

325 315

326 316

327 317

328 318

329 319

330 320

331 321

332 322

333 323

334 324

335 325

336 326

337 327

338 328

339 329

340 330

341 331

342 332

343 333

344 334

345 335

346 336

347 337

348 338

349 339

350 340

351 341

352 342

353 343

354 344

355 345

356 346

357 347

358 348

359 349

360 350

361 351

362 352

363 353

364 354

365 355

366 356

367 357

368 358

369 359

370 360

371 361

372 362

373 363

374 364

375 365

376 366

377 367

378 368

379 369

380 370

381 371

382 372

383 373

384 374

385 375

386 376

387 377

388 378

389 379

390 380

391 381

392 382

393 383

394 384

395 385

396 386

397 387

398 388

399 389

400 390

401 391

402 392

403 393

404 394

405 395

406 396

407 397

408 398

409 399

410 400

411 401

412 402

413 403

414 404

415 405

416 406

417 407

418 408

419 409

420 410

421 411

422 412

423 413

424 414

425 415

426 416

427 417

428 418

429 419

430 420

431 421

432 422

433 423

434 424

435 425

436 426

437 427

438 428

439 429

440 430

441 431

442 432

443 433

444 434

445 435

446 436

447 437

448 438

449 439

450 440

451 441

452 442

453 443

454 444

455 445

456 446

457 447

458 448

459 449

460 450

461 451

462 452

463 453

464 454

465 455

466 456

467 457

468 458

469 459

470 460

471 461

472 462

473 463

474 464

475 465

476 466

477 467

478 468

479 469

480 470

481 471

482 472

483 473

484 474

485 475

486 476

487 477

488 478

489 479

490 480

491 481

492 482

493 483

494 484

495 485

496 486

497 487

498 488

499 489

500 490

501 491

502 492

503 493

504 494

505 495

506 496

507 497

508 498

509 499

510 500

511 501

512 502

513 503

514 504

515 505

516 506

517 507

518 508

519 509

520 510

521 511

522 512

523 513

524 514

525 515

526 516

527 517

528 518

529 519

530 520

531 521

532 522

533 523

534 524

535 525

536 526

537 527

538 528

539 529

540 530

541 531

542 532

543 533

544 534

545 535

546 536

547 537

548 538

549 539

550 540

551 541

552 542

553 543

554 544

555 545

556 546

557 547

558 548

559 549

560 550

561 551

562 552

563 553

564 554

565 555

566 556

567 557

568 558

569 559

570 560

571 561

572 562

573 563

574 564

575 565

576 566

577 567

578 568

579 569

580 570

581 571

582 572

583 573

584 574

585 575

Preface

The effective properties of composite materials, such as thermoelastic and conductive, depend upon the nature of many materials’ characteristics, which are needed to account for the composite structure, e.g. particulate or fibre reinforcement, unidirectional plies or multi-layered laminates. Account also must be taken of the resultant anisotropies that are often required when designing three-dimensional engineering components. Indeed, the properties of some constituents can be anisotropic themselves, such as carbon fibres and the individual plies of laminates. The accurate experimental determination of these properties is rarely, if ever, achieved in practice, and this leads on to the need for reliable estimation methods using analytical and/or numerical methods.

It is emphasised here that this book is not intended to be a reference text. The principal objective is to provide readers with a single source for a wealth of analytical methods and explicit formulae that can be used to estimate the effective properties of a wide range of composite types for both undamaged and damaged states. Readers wishing to track in more detail the historical development of composite theory will need to consult the literature, possibly starting with the limited number of references included in this book.

This book has been written over a number of years following the encouragement of the late Professor Anthony Kelly, FRS, CBE, to whom the author owes an enormous debt of gratitude. Professor Kelly was the Chairman of the Panel at the National Physical Laboratory (NPL) that decided, in 1969, that the author, following six months’ probation, could be offered a permanent post. The author now has an Emeritus position at NPL (Senior NPL Fellow) that has enabled continued research on various aspects of material science, and the writing of this book. A much closer relationship developed when, in the early 1980s, we both independently solved a problem considered in Chapter 14. At that point and onwards Professor Kelly, who was then Vice-Chancellor of Surrey University, introduced the author to many theoretical aspects of composite technology, which are included in this book. Of particular note is the development of methods of analysing the effects of fibre fractures and matrix cracks in unidirectionally reinforced composites, extending the pioneering work of colleagues at NPL, which led to the very well-known ACK (Aveston, Cooper, Kelly) theory, developed in 1971, which continues to be widely cited in the literature.

Following the Introduction, Chapter 2of this book introduces and describes in detail many continuum analyses that will be required in later chapters. Chapters 3– 7are concerned with a description of methods of estimating the effective properties of undamaged composite materials, including those reinforced with aligned spheroidal particles. Extensive use is made of the methodology developed by James Clerk Maxwell in his book on electromagnetism, where an ingenious analytical method is used to estimate the effective electrical conductivity of a uniformly distributed assembly of isotropic spherical particles. His result is thought to be the first expression ever developed for an effective property of a composite. His methodology is also extremely powerful and worthy of extensive use in this book.

During service, composite components are often exposed to loadings that are sufficient to cause the formation of microstructural damage such as fibre failures or matrix cracking, which are usually associated with the occurrence of fibre/matrix interface debonding. For laminates, delamination at ply interfaces is an additional form of load-induced damage. The initiation and growth of microstructural damage affects the effective properties of composite materials, which degrade. It is remarkable that the degradation of very many thermoelastic constants is characterised by a single damage dependent function, as will become clear in the book. Sometimes damage mechanisms lead to local stress-transfer within complex structures, which can delay the onset of structural failure during progressive loading. Chapters 8– 14of this book will focus on analytical and semi-analytical methods of predicting both the effect of damage on effective properties and, more importantly, the dependence of effective properties on local loading conditions when using an energy balance approach. Chapters 13and 14concern, respectively, a model of damage development during the fatigue loading of laminates and a model of composite degradation due to environmental damage (in fibres).

Читать дальше
Тёмная тема
Сбросить

Интервал:

Закладка:

Сделать

Похожие книги на «Properties for Design of Composite Structures»

Представляем Вашему вниманию похожие книги на «Properties for Design of Composite Structures» списком для выбора. Мы отобрали схожую по названию и смыслу литературу в надежде предоставить читателям больше вариантов отыскать новые, интересные, ещё непрочитанные произведения.


Отзывы о книге «Properties for Design of Composite Structures»

Обсуждение, отзывы о книге «Properties for Design of Composite Structures» и просто собственные мнения читателей. Оставьте ваши комментарии, напишите, что Вы думаете о произведении, его смысле или главных героях. Укажите что конкретно понравилось, а что нет, и почему Вы так считаете.

x