Category:Mechanics of Aircraft Structures - University of Florida course EAS4200C

English: For files produces by instructors and students at the University of Florida course EAS4200C Mechanics of Aircraft Structures. See related activity at Wikiversity (usernames starting with Eas4200c). The files shuld ideally be categorized in at least one additional topic-specific category

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Airfoil diagrams used in University of Florida course EAS4200C (Mechanics of Aircraft Structures)‎ (25 F)

Media in category "Mechanics of Aircraft Structures - University of Florida course EAS4200C"

The following 172 files are in this category, out of 172 total.

1stdrawingofoct10.svg 569 × 382; 5 KB
2cell.svg 840 × 581; 10 KB
2ndrawingoct10.svg 744 × 1,052; 12 KB
Aero Schem1.jpg 370 × 402; 11 KB
Aero shear flow.jpg 703 × 281; 18 KB
Airfoil abarvsns max.png 560 × 420; 3 KB
Airfoil and stringers.JPG 729 × 636; 22 KB
Area comp.JPG 512 × 384; 13 KB
Area of triangle.JPG 640 × 512; 15 KB
Axial member.jpg 343 × 459; 34 KB
Beam cross section.jpg 281 × 232; 8 KB
Beam deflection.jpg 560 × 420; 41 KB
Beam deflection2.jpg 560 × 420; 45 KB
Beam under bidirectional bending.jpg 1,218 × 652; 44 KB
Bending moment.JPG 800 × 600; 19 KB
Beta alpha approx.svg 744 × 1,052; 7 KB
Bidirectional bending recipe.svg 744 × 1,052; 27 KB
C1P1d1.jpg 224 × 246; 6 KB
Case1HW6.jpg 560 × 420; 16 KB
Case2HW6.jpg 560 × 420; 16 KB
Chapter 1 img 26.jpg 645 × 489; 45 KB
Circle abarvsns max.png 560 × 420; 3 KB
Circle dumbell.JPG 599 × 456; 16 KB
Circle.JPG 451 × 412; 13 KB
Circle1.JPG 1,179 × 758; 25 KB
Circle24steps.jpg 560 × 420; 32 KB
Circular bar.JPG 618 × 200; 9 KB
Circularvschannel.jpg 689 × 465; 9 KB
Closed thin-walled beam.png 349 × 364; 6 KB
Cross product.JPG 640 × 512; 11 KB
CrossSection.jpg 485 × 321; 16 KB
CrossSectionZoom1.jpg 485 × 321; 9 KB
CrossSectionZoom2.jpg 485 × 321; 8 KB
CrossSectionZoom3.jpg 485 × 321; 9 KB
Curved Shear Panel.jpg 366 × 269; 10 KB
Curved.JPG 640 × 512; 20 KB
Cyclic.JPG 640 × 512; 11 KB
Derivation.JPG 640 × 512; 22 KB
Directional.JPG 640 × 512; 11 KB
Distributed loading.jpg 374 × 274; 15 KB
Example FEA 5-1.JPG 250 × 250; 7 KB
FEA 6-1.JPG 300 × 300; 9 KB
FEA 6-2.JPG 300 × 300; 6 KB
FEAeq 6-1.JPG 102 × 24; 2 KB
FEAeq 6-2.JPG 333 × 103; 10 KB
FEAeq 6-3.JPG 103 × 39; 2 KB
Fig1-12-05.jpg 268 × 388; 12 KB
Fig1aero4200c.jpg 493 × 308; 45 KB
Fig2-12-05.jpg 427 × 357; 9 KB
Fig2asd231.jpg 354 × 247; 28 KB
Fig3asd22.jpg 601 × 450; 58 KB
Fig4are0sd.jpg 402 × 278; 27 KB
Fig5asdew1.jpg 715 × 383; 70 KB
Fig6asdqw2.jpg 327 × 358; 50 KB
Fig8asdq1.jpg 387 × 336; 45 KB
Figuremomentofinertia.JPG 808 × 564; 16 KB
Figuremomentofinertia.jpg 808 × 294; 42 KB
Final Aero Pic.JPG 580 × 510; 14 KB
Firstofnov12.svg 744 × 1,052; 8 KB
GraphIvsb.jpg 339 × 211; 8 KB
Hollow Cylinder Torque.jpg 323 × 183; 7 KB
HW2 open.jpg 318 × 174; 6 KB
HW2 paper.jpg 248 × 180; 5 KB
HW2box.jpg 237 × 233; 7 KB
HW2open.jpg 318 × 174; 4 KB
HW2stack.jpg 223 × 124; 3 KB
HW2stringers.jpg 367 × 182; 6 KB
HW3 average area.jpg 263 × 218; 8 KB
HW3 c.JPG 580 × 510; 16 KB
HW3 circle.jpg 316 × 301; 13 KB
HW3 closer look.jpg 352 × 223; 6 KB
HW3 curved panel.jpg 282 × 237; 6 KB
HW3 gamma.jpg 306 × 248; 6 KB
HW3 paper cross.jpg 373 × 360; 11 KB
HW3 triangle area.jpg 409 × 309; 12 KB
HW3 triangle.jpg 242 × 203; 8 KB
HW4 Quadrature.jpg 449 × 365; 20 KB
HW4 rpq.jpg 373 × 292; 10 KB
HW4 shear triangle.jpg 346 × 171; 6 KB
HW4 Trapezoidal.jpg 380 × 221; 7 KB
HW5 2.jpg 560 × 420; 19 KB
HW5 shear.jpg 489 × 379; 19 KB
HW5 triangle.jpg 517 × 357; 13 KB
HW6picture.jpg 585 × 403; 36 KB
HW7 peace1.jpg 320 × 299; 10 KB
HW7 peace2.jpg 285 × 279; 10 KB
HW7 potato isolated.jpg 424 × 403; 21 KB
HW7 potato isolated2.jpg 424 × 403; 20 KB
HW7 stringer 3 iso.jpg 424 × 403; 11 KB
HW7 stringer j.jpg 421 × 319; 11 KB
HW7 stringer j2.jpg 421 × 319; 11 KB
Hwareo2.jpg 502 × 471; 24 KB
I yz circle.JPG 941 × 891; 30 KB
Ibeam for prob3.jpg 271 × 263; 7 KB
IbeamNAxis.jpg 505 × 251; 11 KB
JvsNS.jpg 560 × 420; 13 KB
KcVSab.jpg 560 × 420; 39 KB
Last Aero 1.JPG 761 × 572; 24 KB
Last Aero 2.JPG 761 × 572; 22 KB
Last aero Ever.JPG 999 × 439; 33 KB
Lastone.jpg 560 × 420; 16 KB
Lect12 2.JPG 341 × 177; 9 KB
Lect12 3.JPG 241 × 246; 9 KB
Lect12 4.JPG 158 × 136; 4 KB
Lect12 5.JPG 413 × 240; 12 KB
Lect12 6.JPG 312 × 215; 9 KB
Lect18 1.JPG 398 × 214; 16 KB
Lect18 2.JPG 398 × 214; 7 KB
Lect30 1.JPG 329 × 309; 9 KB
Lect30 2.JPG 329 × 309; 10 KB
Lect36 1.JPG 294 × 311; 12 KB
Lect36 2.JPG 229 × 282; 9 KB
Lect36 3.JPG 220 × 276; 8 KB
Lect36 4.JPG 229 × 282; 9 KB
Magicman1.JPG 967 × 502; 25 KB
Mohr's circle aero.JPG 2,048 × 1,536; 963 KB
Mohr'sCircle.JPG 759 × 604; 24 KB
MohrCircle.SVG 512 × 423; 2 KB
MomentofInertia.jpg 197 × 234; 6 KB
Multi-Celled.JPG 911 × 730; 33 KB
Multicell problem.jpg 686 × 385; 29 KB
Non-circular.jpg 640 × 400; 20 KB
Non-uniform stress field 3D.jpg 372 × 293; 14 KB
Onecircle.JPG 640 × 512; 13 KB
Open Thin Walled.jpg 373 × 360; 12 KB
Parallel Axis.JPG 2,048 × 1,536; 936 KB
Quadrature.JPG 512 × 384; 25 KB
Radsam Airfoil abarvsns max.png 560 × 420; 3 KB
Rec plate.jpg 483 × 339; 14 KB
RecAirfoil.jpg 560 × 420; 14 KB
Rectangle1.JPG 1,179 × 758; 25 KB
Rectangular axis beam.jpg 2,048 × 1,536; 955 KB
Rectangular Beam.jpg 800 × 600; 24 KB
Rectangular Box Beam.jpg 800 × 600; 24 KB
Ricardoalbuquerquehwpic.jpg 526 × 615; 31 KB
Rotation of the cross-section of a bar.jpg 488 × 301; 15 KB
S-curve.jpg 500 × 440; 15 KB
Seconddrawingofnov12.svg 744 × 1,052; 18 KB
Section.JPG 512 × 384; 19 KB
Shear deformation.JPG 363 × 301; 9 KB
Shear Force in Shear Flow.jpg 1,154 × 443; 17 KB
Shear force in shear flow.png 633 × 465; 14 KB
Shear on box.jpg 262 × 234; 6 KB
Shear Panel.jpg 324 × 162; 8 KB
SigxxVSyBF.jpg 560 × 420; 16 KB
SigxxVSyEH.jpg 560 × 420; 16 KB
Single-cell box with four stringers.svg 744 × 1,052; 39 KB
Solid Circular CS.JPG 729 × 636; 20 KB
Solid CS.JPG 729 × 636; 26 KB
Squarebarbell.jpg 689 × 465; 9 KB
Stacking example.JPG 788 × 359; 28 KB
StepsVSarea.jpg 560 × 420; 15 KB
StepsVSareaAirfoil.jpg 560 × 420; 17 KB
StepsVSerror.jpg 560 × 420; 17 KB
StepsVSerrorAirfoil.jpg 560 × 420; 16 KB
Stiff2.jpg 414 × 402; 11 KB
Stringer x-sec.JPG 759 × 604; 22 KB
Structeq-6-1.JPG 444 × 53; 6 KB
Thin wall shear distribution assumption.jpg 574 × 224; 18 KB
Thin walled beam.JPG 577 × 337; 10 KB
Thin walled beams.jpg 589 × 245; 13 KB
Thin-wall.JPG 640 × 512; 17 KB
Twist.JPG 640 × 512; 20 KB
Two force members.jpg 417 × 251; 7 KB
Two-cell.jpg 640 × 400; 22 KB
TwoBeams.JPG 759 × 604; 23 KB
Uniaxial stress new.jpg 530 × 233; 13 KB
Uniaxial stress.jpg 530 × 233; 13 KB
Uniaxial tension.JPG 540 × 257; 8 KB
Uniform Circular.png 1,472 × 800; 315 KB
Uniform vs. non-uniform loading.jpg 735 × 356; 40 KB
Vu.JPG 640 × 512; 11 KB

Category:Mechanics of Aircraft Structures - University of Florida course EAS4200C

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Media in category "Mechanics of Aircraft Structures - University of Florida course EAS4200C"

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