Books on the topic 'Axial loads'

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1

Li︠a︡tkher, V. M. Seismic loads. Hoboken, New Jersey: John Wiley & Sons, Inc., 2016.

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2

Danielson, D. A. Analytical tripping loads for stiffened plates. Monterey, Calif: Naval Postgraduate School, 1994.

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3

Gur, J. Ari. Experimental studies with metal plates subjected to inplane axial impact. Haifa: Technion Israel Institute of Technology, 1985.

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4

Design of highly loaded axial-flow fans and compressors. White River Junction, Vt: Concepts ETI, 2000.

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5

Tennyson, Roderick C. Buckling of composite cylinders under axial compression. Amsterdam: Elsevier, 1987.

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6

United States. National Aeronautics and Space Administration., ed. Axisymmetric deformations and stresses of unsymmetrically laminated composite cylinders in axial compression with thermally-induced preloading effects. Bethesda, MD: Carderock Division, Naval Surface Warfare Center, 1993.

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7

Tennyson, Roderick C. Buckling of imperfect sandwich cylinders under axial compression. [S.l.]: [s.n.], 1990.

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8

Tom, Cordes, Lease Kevin, and Society of Automotive Engineers. Fatigue Design and Evaluation Committee., eds. Multiaxial fatigue of an induction hardened shaft. Warrendale, Pennsylvania: SAE, 1999.

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9

Cheung, E. W. Buckling of composite sandwich cylinders under axial compression. Amsterdam: Elsevier Science Publishers, 1988.

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10

Cheung, Eric Waihon. Buckling of composite sandwich cylinders under axial compression. [Downsview, Ont.]: Dept. of Aerospace Science and Engineering, University of Toronto, 1988.

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11

Bornsteiln, A. Vibration and buckling tests of stringer-stiffened cylindrical shells subjected to non-uniform axial loading. Haifa, Israel: Technion - Israel Institute of Technology, 1991.

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12

Sun, Guojun. Optimal design of laminated-composite circular-cylindrical shells subjected to combined loads. [S.l.]: American Society of Mechanical Engineers, 1988.

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13

Ho, Gordon. Nonlinear analysis of reinforced concrete beams subjected to shear, moment and axial loads. Ottawa: National Library of Canada, 1993.

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14

Sreeramesh, Kalluri, Bonacuse Peter J. 1960-, and Symposium on Multiaxial Fatigue and Deformation: Testing and Prediction (1999 : Seattle, Wash.), eds. Multiaxial fatigue and deformation: Testing and prediction. W. Conshohocken, PA: ASTM, 2000.

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15

Gotsis, Pascal K. Progressive fracture of fiber composite thin shell structures under internal pressure and axial loads. [Washington, DC]: National Aeronautics and Space Administration, 1996.

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16

Gotsis, Pascal K. Progressive fracture of fiber composite thin shell structures under internal pressure and axial loads. [Washington, DC]: National Aeronautics and Space Administration, 1996.

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17

S, Dhadwal Harbans, and NASA Glenn Research Center, eds. Simultaneous optical measurements of axial and tangential steady-state blade deflections. [Cleveland, Ohio]: National Aeronautics and Space Administration, Glenn Research Center, 1999.

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18

S, Dhadwal Harbans, and NASA Glenn Research Center, eds. Simultaneous optical measurements of axial and tangential steady-state blade deflections. [Cleveland, Ohio]: National Aeronautics and Space Administration, Glenn Research Center, 1999.

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19

Paul, J. Analysis and repair of impact damaged composites (U). Melbourne, Victoria, Australia: Aeronautical Research Laboratory, 1989.

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20

Nemeth, Michael P. Buckling behavior of long symmetrically laminated plates subjected to shear and linearly varying axial edge loads. Washington, D.C: National Aeronautics and Space Administration, 1997.

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21

Dowling, Norman E. J-integral estimates for cracks in infinite bodies. [Washington, D.C.]: National Aeronautics and Space Administration, 1986.

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22

W, Tam C. K., and United States. National Aeronautics and Space Administration., eds. Numerical simulation of the generation of axisymmetric mode jet screech tones. Reston, Va: American Institute of Aeronautics and Astronautics, 1998.

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23

W, Tam C. K., and United States. National Aeronautics and Space Administration., eds. Numerical simulation of the generation of axisymmetric mode jet screech tones. Reston, Va: American Institute of Aeronautics and Astronautics, 1998.

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24

C, Chamis C., Minnetyan L, and United States. National Aeronautics and Space Administration., eds. Computational simulation of damage progression of composite thin shells subjected to mechanical loads. [Washington, D.C: National Aeronautics and Space Administration, 1996.

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25

Ginder, John. A new look at the analytical problem of the buckling of anisotropic circular cylindrical shells under axial compresssion. [Downsview, Ont.]: Dept. of Aerospace Science and Engineering, 1987.

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26

Center, NASA Glenn Research, ed. Derivation of the data reduction equations for the calibration of the six-component thrust stand in the CE-22 advanced nozzle test facility. [Cleveland, Ohio]: National Aeronautics and Space Administration, Glenn Research Center, 2003.

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27

Karl, Owen A., and United States. National Aeronautics and Space Administration., eds. Forced response testing of an axi-centrifugal turboshaft engine. [Washington, D.C: National Aeronautics and Space Administration, 1996.

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28

Hyer, M. W. Innovative design of composite structures: Axisymmetric deformations of unsymmetrically laminated cylinders loaded in axial compression : semiannual status report. Blacksburg, Va: College of Engineering, Virginia Polytechnic Institute and State University, 1990.

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29

J, Minguet Pierre, O'Brien T. Kevin, and Langley Research Center, eds. A method for calculating strain energy release rates in preliminary design of composite skin/stringer debonding under multi-axial loading. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1999.

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30

F, Card Michael, and United States. National Aeronautics and Space Administration., eds. Effects of stiffening and mechanical load on thermal buckling of stiffened cylindrical shells: Presented at the AIAA/ASCE/ASC 36th Structures, Structural Dynamics and Materials Conference, April 10-12, 1995, New Orleans, LA, Thermal Structures Category. [Washington, D.C: National Aeronautics and Space Administration, 1995.

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31

M, Kwaśniewski, Li Xiaochun 1964-, and Takahashi Manabu 1955-, eds. True triaxial testing of rocks. Boca Raton, FL: CRC Press/Balkema, 2012.

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32

Verderaime, V. Plate and butt-weld stresses beyond elastic limit, material and structural modeling. Marshall Space Flight Center, Ala: George C. Marshall Space Flight Center, 1991.

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33

George C. Marshall Space Flight Center., ed. Plate and butt-weld stresses beyond elastic limit, material and structural modeling. Washington, D.C: National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division, 1991.

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34

Yang, L. Behaviour of masonry columns of geometric section subjected to eccentric axial load. Manchester: UMIST, 1995.

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35

1945-, Sharma Om P., and United States. National Aeronautics and Space Administration., eds. Impact of periodic unsteadiness on performance and heat load in axial flow turbomachines. [Washington, D.C.]: National Aeronautics and Space Administration, 1997.

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36

Kiencke, U. Automotive control systems. Berlin: Springer, 2000.

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37

Petsios, Mikhalis. Buckling of thin truncated conical shells (Frusta) under quasi-static and dynamic axial load. Manchester: UMIST, 1993.

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38

Lyatkher, Victor M. Seismic Loads. Wiley & Sons, Incorporated, John, 2015.

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39

Lyatkher, Victor M. Seismic Loads. Wiley & Sons, Incorporated, John, 2015.

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40

Lyatkher, Victor M. Seismic Loads. Wiley & Sons, Limited, John, 2015.

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41

Lyatkher, Victor M. Seismic Loads. Wiley & Sons, Incorporated, John, 2015.

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42

Society of Automotive Engineers Fatigue Design and Evaluation committe (Corporate Author), Tom Cordes (Editor), and Kevin Lease (Editor), eds. Multiaxial Fatigue of an Induction Hardened Shaft: Ae-28 (Ae (Series)). Society of Automotive Engineers Inc, 1999.

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43

Structural Engineering Institute (Corporate Author), ed. Design Live Loads for Parking Garages: A Report to the Structural Engineering Institute of the American Society of Civil Engineers. Amer Society of Civil Engineers, 2000.

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44

Loads simulation and analysis in automotive engineering. Warrendale, PA: Society of Automotive Engineers, 2004.

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45

Engineers, Society of Automotive, and SAE World Congress (2005 : Detroit, Mich.), eds. Loads simulation and analysis in automotive engineering. Warrendale, Pa: SAE International, 2005.

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46

Institution of Mechanical Engineers (Great Britain). Fluid Machinery Committee., ed. Radial loads and axial thrusts on centrifugal pumps: Papers presented at a seminar. London: The Institution, 1986.

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47

Determination of the ultimate capacity of elastomeric bearings under axial loading: A report to U.S. Department of Commerce, Technology Administration, National Institute of Standards and Technology, Building and Fire Research Laboratory. Gaithersburg, MD: The Institute, 1998.

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48

Determination of the ultimate capacity of elastomeric bearings under axial loading: A report to U.S. Department of Commerce, Technology Administration, National Institute of Standards and Technology, Building and Fire Research Laboratory. Gaithersburg, MD: The Institute, 1998.

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49

C, Chang Peter, Taylor A. W, and National Institute of Standards and Technology (U.S.), eds. Determination of the ultimate capacity of elastomeric bearings under axial loading: A report to U.S. Department of Commerce, Technology Administration, National Institute of Standards and Technology, Building and Fire Research Laboratory. Gaithersburg, MD: The Institute, 1998.

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50

Center, Langley Research, ed. Buckling behavior of long symmetrically laminated plates subjected to shear and linearly varying axial edge loads. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1997.

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