Table 9 Effect of parameter \(\:{\varvec{K}}_{1}\) on the changes of frequencies of the sandwich curved beam with changes of thermal loads.

From: A unified multifield formulation for analysis of a sandwich graphene origami reinforced composite curved structure

\(\:{T(}^{O}K)\)

\(\:{K}_{1}=0\)

\(\:{K}_{1}=1\times\:{10}^{7}\)

\(\:{K}_{1}=2\times\:{10}^{7}\)

\(\:{K}_{1}=3\times\:{10}^{7}\)

320

36.48141

36.53733

36.59343

36.64854

325

36.48093

36.53695

36.59272

36.64839

330

36.48044

36.53657

36.59200

36.64824

335

36.47996

36.53619

36.59129

36.64809

340

36.47947

36.53581

36.59058

36.64794

345

36.47931

36.53484

36.58987

36.64779

350

36.47914

36.53387

36.58916

36.64764

355

36.47898

36.53289

36.58845

36.64749

360

36.47881

36.53192

36.58836

36.64644

365

36.47822

36.53095

36.58823

36.64629

370

36.47763

36.52998

36.58809

36.64614

375

36.47704

36.52900

36.58796

36.64599

380

36.47646

36.52803

36.58782

36.64475

385

36.47574

36.52706

36.58768

36.64460

390

36.47503

36.52609

36.58755

36.64445

395

36.47431

36.52512

36.58741

36.64430

400

36.4736

36.52415

36.58728

36.64402

405

36.47323

36.52318

36.58714

36.64402

410

36.47287

36.52221

36.58701

36.64402

415

36.47251

36.52123

36.58687

36.64402

420

36.47215

36.52026

36.58674

36.64402