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Books on the topic 'Axial loads'

Author: Grafiati
Published: 4 June 2021
Last updated: 25 July 2025

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1

Li︠a︡tkher, V. M. Seismic loads. John Wiley & Sons, Inc., 2016.

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2

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

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3

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

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4

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. Carderock Division, Naval Surface Warfare Center, 1993.

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5

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

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6

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

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7

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

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8

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

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9

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

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10

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

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11

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

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12

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. ASTM, 2000.

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13

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

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14

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

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15

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

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16

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

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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. 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. National Aeronautics and Space Administration, Glenn Research Center, 1999.

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19

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

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20

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

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21

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. The Institute, 1998.

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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. 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. American Institute of Aeronautics and Astronautics, 1998.

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24

Dowling, Norman E. J-integral estimates for cracks in infinite bodies. National Aeronautics and Space Administration, 1986.

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25

United States. National Aeronautics and Space Administration., ed. J-integral estimates for cracks in infinite bodies. National Aeronautics and Space Administration, 1986.

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26

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

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27

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

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28

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

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29

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. National Aeronautics and Space Administration, 1996.

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30

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. National Aeronautics and Space Administration, 1996.

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31

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. National Aeronautics and Space Administration, Glenn Research Center, 2003.

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32

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

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33

Center, Langley Research, ed. Fracture analysis of stiffened panels under biaxial loading with widespread cracking. National Aeronautics and Space Administration, Langley Research Center, 1995.

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34

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

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35

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. National Aeronautics and Space Administration, Langley Research Center, 1999.

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36

Ya, Timofeev I., Shipilov S. D, and United States. National Aeronautics and Space Administration., eds. Calculation of the distributed loads on the blades of individual multiblade propellers in axial flow using linear and nonlinear lifting surface theories. National Aeronautics and Space Administration, 1988.

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37

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. National Aeronautics and Space Administration, 1995.

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38

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. National Aeronautics and Space Administration, 1995.

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39

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

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40

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

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41

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

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42

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

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43

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

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44

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

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45

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

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46

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. National Aeronautics and Space Administration, 1997.

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47

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

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48

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

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49

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

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50

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

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