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Books on the topic 'Structural weight'

Author: Grafiati

Published: 4 June 2021

Last updated: 27 July 2025

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1

Rees, D. W. A. Mechanics of optimal structural design: Minimum weight structures. J. Wiley, 2009.

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Rees, D. W. A. Mechanics of optimal structural design: Minimum weight structures. J. Wiley, 2009.

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3

N, Patnaik Surya, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Program., eds. Weight minimization of structural components for launch in space shuttle. National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program, 1994.

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4

United States. National Aeronautics and Space Administration., ed. Minimum weight design of a generic axisymmetric inlet. National Aeronautics and Space Administration, 1996.

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5

International Conference on Steel and Aluminium Structures (4th 1999 Espoo, Finland). Light-weight steel and aluminium structures: Fourth International Conference on Steel and Aluminium Structures. Elsevier, 1999.

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6

United States. National Aeronautics and Space Administration. Scientific and Technical Information Office., ed. Preliminary structural design of composite main rotor blades for minimum weight. National Aeronautics and Space Administration, Scientific and Technical Information Office, 1987.

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7

Culpepper, Steven Drew. Structural considerations for aircraft payload modification-P-3H zero fuel weight increase. Naval Postgraduate School, 1991.

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8

International Conference on Steel and Aluminium Structures (4th 1999 Espoo, Finland). Light-weight steel and aluminium structures: Fourth International Conference on Steel and Aluminium Structures, Espoo, Finland, 20-23 June 1999. Elsevier, 1999.

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9

Jefferson, Stroud W., and United States. National Aeronautics and Space Administration. Scientific and Technical Information Program., eds. Effect of bow-type initial imperfection on reliability of minimum-weight, stiffened structural panels. National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program, 1993.

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10

Stroud, W. Jefferson. Effect of bow-type initial imperfection on reliability of minimum-weight, stiffened structural panels. Langley Research Center, 1993.

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11

Jefferson, Stroud W., and United States. National Aeronautics and Space Administration. Scientific and Technical Information Program., eds. Effect of bow-type initial imperfection on reliability of minimum-weight, stiffened structural panels. National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program, 1993.

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12

Ardema, Mark D. Advanced methods of structural and trajectory analysis for transport aircraft: Final report, June 15, 1994 - September 30, 1995. Santa Clara University, 1995.

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13

United States. National Aeronautics and Space Administration., ed. Advanced methods of structural and trajectory analysis for transport aircraft: Final report, June 15, 1994 - September 30, 1995. Santa Clara University, 1995.

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14

Ardema, Mark D. Development of advanced methods of trajectory and structural analysis for hypersonic aircraft: Final report, October 1, 1995 - January 31, 1997, NASA Ames Research Center grant NCC2-5165. National Aeronautics and Space Administration, 1997.

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15

United States. National Aeronautics and Space Administration., ed. Development of advanced methods of trajectory and structural analysis for hypersonic aircraft: Final report, October 1, 1995 - January 31, 1997, NASA Ames Research Center grant NCC2-5165. National Aeronautics and Space Administration, 1997.

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16

Fan, Mark S. Structural design and analysis of a light-weight laminated composite heat sink for spaceflight PWBs. National Aeronautics and Space Administration, 1997.

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17

Saravanos, D. A. Multi-objective shape and material optimization of composite structures including damping. NASA, 1990.

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18

C, Chamis C., and United States. National Aeronautics and Space Administration., eds. Multi-objective shape and material optimization of composite structures including damping. NASA, 1990.

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19

C, Chamis C., and United States. National Aeronautics and Space Administration., eds. Multi-objective shape and material optimization of composite structures including damping. NASA, 1990.

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20

Morales-Valentin, Gustavo E. Temperature differential effect on the falling weight deflectometer deflections used for structural evaluation of rigid pavements. Center for Transportation Research, Bureau of Engineering Research, University of Texas at Austin, 1987.

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21

United States. National Aeronautics and Space Administration., ed. A class II weight assessment for the implementation of commonality and preliminary structural designs for the family of commuter airplanes. National Aeronautics and Space Administration, 1987.

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22

United States. National Aeronautics and Space Administration., ed. Electrochemical impregnation and cycle life of lightweight nickel electrodes for nickel-hydrogen cells. National Aeronautics and Space Administration, 1990.

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23

United States. National Aeronautics and Space Administration., ed. Development of advanced methods of structural and trajectory analysis for transport aircraft: Final report : October 1, 1995-February 28, 1998 : NASA Ames Research Center grant NCC2-5167. National Aeronautics and Space Administration, 1998.

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24

Ardema, Mark D. Development of advanced methods of structural and trajectory analysis for transport aircraft: Annual report : October 1, 1995 - September 30, 1996. Santa Clara University, 1996.

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25

United States. National Aeronautics and Space Administration., ed. Development of advanced methods of structural and trajectory analysis for transport aircraft: Annual report : October 1, 1995 - September 30, 1996. Santa Clara University, 1996.

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26

Diefenderfer, Brian K. Network-level pavement evaluation of Virginia's interstate system using the falling weight deflectometer. Virginia Transportation Research Council, 2008.

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27

Williamson, Thomas James. Weight optimum arch structures. Naval Postgraduate School, 1992.

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28

Menzies, Margaret Anne. Weight optimum arch structures. Naval Postgraduate School, 1991.

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29

Duffy, Stephen F. Design protocols and analytical strategies that incorporate structural reliability models: Final report; reporting period: January 19, 1996 - January 18, 1997; grant number: NASA cooperative agreement NCC 3-448. National Aeronautics and Space Administration, 1997.

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30

Santillan-Ortega, R. Design of light weight composite vehicle structures. UMIST, 1996.

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31

W, Lee Eui, Minerals, Metals and Materials Society. Non-ferrous Metals Committee., and Minerals, Metals and Materials Society. Meeting, eds. Light weight alloys for aerospace applications IV: Proceedings of the fourth "Light weight alloys for aerospace applications" symposium : sponsored by the Non-Ferrous Metals Committee of the Structural Materials Division (SMD) of the Minerals, Metals & Materials Society (TMS), held February 10-13, 1997, TMS Annual Meeting in Orlando, Florida. Minerals, Metals & Materials Society, 1997.

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32

Parker, Victoria. How tall is tall?: Comparing structures. Raintree, 2012.

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33

Parker, Victoria. How tall is tall?: Comparing structures. Heinemann Library, 2011.

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34

Parker, Victoria. How tall is tall?: Comparing structures. Heinemann Library, 2011.

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35

J, Horn Walter, Ritter James, and Langley Research Center, eds. Weight estimation techniques for composite airplanes in general aviation industry. National Aeronautics and Space Administration, Langley Research Center, 1986.

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36

Daniels, H. A. M. A CAD-system for the design of stiffened panels in wing box structures. National Aerospace Laboratory, 1985.

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37

El-Gindy, Moustafa. Influence of a trailer's axle arrangement and loads on the stability and control of a tractor/semitrailer. Federal Highway Administration, 1998.

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38

Author, Pincus Philip A., ed. Structured fluids: Polymers, colloids, surfactants : XD-US. Oxford University Press, 2010.

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39

Chang-Qing, Hu, Shu Chi-Wang, and Institute for Computer Applications in Science and Engineering., eds. A technique of treating negative weights in WENO schemes. Institute for Computer Applications in Science and Engineering, NASA Langley Research Center, 2000.

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40

Rees, David W. A. Mechanics of Optimal Structural Design: Minimum Weight Structures. Wiley & Sons, Incorporated, John, 2009.

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41

Rees, David. Mechanics of Optimal Structural Design: Minimum Weight Structures. Wiley & Sons, Limited, John, 2009.

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42

Bianconi, Ginestra. Structural Correlations of Multiplex Networks. Oxford University Press, 2018. http://dx.doi.org/10.1093/oso/9780198753919.003.0007.

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Multiplex networks encode relevant information in their correlated structure, including interlayer degree correlation, link overlap, weight–topology correlations in weighted multiplex networks and activity of the nodes. Interlayer degree correlations among a pair of layers indicates for instance whether or not the hub nodes of one layer are also hub nodes in the other. Link overlap indicates that a finite fraction of nodes are connected in more than one layer. Weight–topology correlations of weighted complex networks reveal that the weight of the links is not random, but often correlated with

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43

Innovative Structural Materials: Reducing Weight of Transportation Equipment. Springer, 2023.

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44

A rapid empirical method for estimating the gross takeoff weight of a high speed civil transport. National Aeronautics and Space Administration, Langley Research Center, 1999.

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45

A rapid empirical method for estimating the gross takeoff weight of a high speed civil transport. National Aeronautics and Space Administration, Langley Research Center, 1999.

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46

P. Mäkeläinen (Editor) and P. Hassinen (Editor), eds. Light-Weight Steel and Aluminium Structures. Elsevier Science, 1999.

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47

P. Mäkeläinen (Editor) and P. Hassinen (Editor), eds. Light-Weight Steel and Aluminium Structures. Elsevier Science, 1999.

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48

Weight optimization of an aerobrake structural concept for a lunar transfer vehicle. National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program, 1992.

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49

Henriksen, Marius, Robin Christensen, Berit L. Heitmann, and Henning Bliddal. Weight loss. Oxford University Press, 2016. http://dx.doi.org/10.1093/med/9780199668847.003.0023.

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Obesity is widely acknowledged as a risk factor for both the incidence and progression of osteoarthritis. Loss of at least 10% of body weight is recognized as a cornerstone in the management of obese patients with osteoarthritis, and can lead to significant improvement in symptoms, pain relief, physical function, and health-related quality of life. However, questions still remain surrounding optimal management and whether structural disease progression can be arrested. Given the significant health, social, and economic burden of osteoarthritis, especially in obese patients, it is imperative to

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50

Hemp, W. S., H. L. Cox, and R. L. Bisplinghoff. Design of Structures of Least Weight : International Series of Monographs in Aeronautics and Astronautics: Solid and Structural Mechanics, Vol. 8. Elsevier Science & Technology Books, 2014.

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