Książki na temat „Axial loads”

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

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

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

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

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

United States. National Aeronautics and Space Administration., red. 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.

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

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

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

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

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.

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

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

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

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.

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.

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

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

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

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.

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

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

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

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

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.

Center, NASA Glenn Research, red. 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.

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

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.

J, Minguet Pierre, O'Brien T. Kevin i Langley Research Center, red. 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.

F, Card Michael, i United States. National Aeronautics and Space Administration., red. 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.

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

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.

George C. Marshall Space Flight Center., red. 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.

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

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

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

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

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

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

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

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

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

Structural Engineering Institute (Corporate Author), red. 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.

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

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

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

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.

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.

C, Chang Peter, Taylor A. W i National Institute of Standards and Technology (U.S.), red. 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.

Center, Langley Research, red. 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.