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Books on the topic 'Method of deformable configurations'

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Published: 30 May 2022

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1

Dale, Bryan Richard. A shear deformable finite element for laminated plates. [Downsview, Ont.]: Dept. of Aerospace Science and Engineering, 1987.

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2

Bazhlekov, Ivan Blagoev. Non-singular boundary-integral method for deformable drops in viscous flows. Eindhoven: Technische Universiteit Eindhoven, 2003.

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3

Ueda, Tetsuhiko. Unsteady aerodynamic calculations for general configurations by the doublet-point method. Tokyo, Japan: National Aerospace Laboratory, 1991.

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4

Barger, Raymond L. A method for designing blended wing-body configurations for low wave drag. [Washington, DC]: National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program, 1992.

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5

Hounjet, M. H. L. ARSPNSC: A method to calculate subsonic steady and unsteady potential flow about complex configurations. Amsterdam: National Aerospace Laboratory, 1986.

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6

Uosukainen, Seppo. JMC method applied to active control of sound: Theoretical extensions and new source configurations. Espoo [Finland]: Technical Research Centre of Finland, 1999.

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7

Obeid, Amneh Abdullah Ahmed. Magnet implant system configurations: A method of optimising the effeciency of complete mandibular overdentures. Birmingham: University of Birmingham, 1997.

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8

Gordon, Royle, and Whittle Geoff 1950-, eds. The internally 4-connected binary matroids with no M(K3,3)-minor. Providence, R.I: American Mathematical Society, 2010.

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9

Hounjet, M. H. L. CAR 88: A method to calculate subsonic and supersonic, steady and unsteady, potential flow about complex configurations. Amsterdam: National Aerospace Laboratory, 1988.

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10

1961-, Joskowicz Leo, ed. The configuration space method for kinematic design of mechanisms. Cambridge, Mass: MIT Press, 2010.

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11

Beek, C. M. van. Development of an advanced panel method for complex configurations in subsonic compressible flow; application to the computation of the potential flow through ducts. Amsterdam, Netherlands: National Aerospace Laboratory, 1987.

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12

Iollo, Angelo. Pseudo-time method for optimal shape design using the Euler equations. Hampton, Va: Institute for Computer Applications in Science and Engineering, 1995.

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13

Frink, Neal T. Tetrahedral finite-volume solutions to the Navier-Stokes equations on complex configurations. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1998.

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14

Peters, M. E. A user's manual for the method of moments Aircraft Modeling Code (AMC). Hampton, VA: National Aeronautics and Space Administration, Langley Research Center, 1989.

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15

Chattopadhyay, Aditi. Development of multiobjective optimization techniques for sonic boom minimization: Final report on NASA Ames grant no. NCC2-5064, performance period--5/16/94-9/15/96. [Washington, DC: National Aeronautics and Space Administration, 1996.

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16

Chattopadhyay, Aditi. Development of multiobjective optimization techniques for sonic boom minimization. [Washington, D.C: National Aeronautics and Space Administration, 1995.

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17

Hamed, A. Probabilistic modeling for simulation of aerodynamic uncertainties in propulsion systems. [Washington, D.C.]: National Aeronautics and Space Administration, 1989.

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18

Applin, Zachary T. Experimental and theoretical aerodynamic characteristics of a high-lift semispan wing model. [Washington, D.C.]: National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division, 1990.

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19

Busacca, Maurizio, and Roberto Paladini. Collaboration Age. Venice: Fondazione Università Ca’ Foscari, 2020. http://dx.doi.org/10.30687/978-88-6969-424-0.

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Abstract:
Recently, public policies of urban regeneration have intensified and multiplied. They are being promoted with the aim to start social and economic dynamics within the local context which is subject to intervention. From the empirical analysis, we realise that such activities are mainly implemented by three subjects or by mixed coalitions (public institutions, actors of the third sector and companies). Within them, each player is moved by a multiplicity of interests and goals that go beyond their own nature – public interest, market and mutualism – and tend to redefine themselves, thus becoming hybrid forms of production of value (social, economic, cultural). By studying a number Italian and Catalan cases, this essay deals with the theory that, under specific conditions and configurations, a collaborative direction – of organization, production and design – would give life to successful procedures, even without the identification of a one-best-way. The collaboration is not simply a choice of operation, but a real production method which mobilises social resources to create hybrid solutions – between state, market and society – to complex issues that could not be faced solely with the use of the rationale of action of one among the three actors. In this framework, the systems of relations and interactions between players and shared capital become an essential condition for the success of every initiative of urban redevelopment, or failure thereof. Such initiatives are brought to life by the strategic role of individuals who foster connections as well as the dissemination of non-redundant information between social networks, and collective and individual actors which would otherwise be separated and barely able to communicate and collaborate with each other. In addition to the functions carried out by knowledge brokers, that have been extensively described in organisational studies and economic sociology, the aforementioned figures act as real social enzymes, that is to say, they handle the available information and function as catalysts of social processes of production of knowledge. Moreover, they increase the reaction speed, working on mechanisms which control the spontaneity.
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20

1952-, Campbell Richard L., and United States. National Aeronautics and Space Administration. Scientific and Technical Information Program., eds. Applications of a direct/iterative design method to complex transonic configurations. [Washington, DC]: National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program, 1992.

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21

Applications of a direct/iterative design method to complex transonic configurations. [Washington, DC]: National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program, 1992.

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22

B, Fichter W., and Langley Research Center, eds. A finite-element alternating method for two-dimensional mode-I crack configurations. Hampton, Va: National Aeronautics ansd Space Administration, Langley Research Center, 1988.

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23

B, Fichter W., and Langley Research Center, eds. A finite-element alternating method for two-dimensional mode-I crack configurations. Hampton, Va: National Aeronautics ansd Space Administration, Langley Research Center, 1988.

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24

A finite-element alternating method for two-dimensional mode-I crack configurations. Hampton, Va: National Aeronautics ansd Space Administration, Langley Research Center, 1988.

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25

Joskowicz, Leo, and Elisha Sacks. Configuration Space Method for Kinematic Design of Mechanisms. MIT Press, 2010.

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26

Joskowicz, Leo, and Elisha Sacks. Configuration Space Method for Kinematic Design of Mechanisms. MIT Press, 2018.

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27

Joskowicz, Leo, and Elisha Sacks. Configuration Space Method for Kinematic Design of Mechanisms. MIT Press, 2010.

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28

C, Taylor Arthur, Barnwell Richard W, and United States. National Aeronautics and Space Administration., eds. Aerodynamic shape sensitivity analysis and design optimization of complex configurations using unstructured grids. [Washington, DC: National Aeronautics and Space Administration, 1997.

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29

Aerodynamic shape sensitivity analysis and design optimization of complex configurations using unstructured grids. [Washington, DC: National Aeronautics and Space Administration, 1997.

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30

United States. National Aeronautics and Space Administration. Scientific and Technical Information Division., ed. An algebraic homotopy method for generating quasi-three-dimensional grids for high-speed configurations. [Washington, DC]: National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division, 1989.

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31

E, Needleman Kathy, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Division., eds. A semiempirical method for obtaining fuselage normal areas from fuselage mach sliced areas. [Washington, DC]: National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division, 1990.

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32

1964-, Hartley T. T., and Lewis Research Center, eds. A method for generating reduced-order linear models of multidimensional supersonic inlets. [Cleveland, Ohio]: National Aeronautics and Space Administration, Lewis Research Center, 1998.

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33

Geojoe, Kuruvila, Ta'asan Shlomo, and Institute for Computer Applications in Science and Engineering., eds. Pseudo-time method for optimal shape design using the Euler equations. Hampton, VA: Institute for Computer Applications in Science and Engineering, NASA Langley Research Center, 1995.

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34

Geojoe, Kuruvila, Ta'asan Shlomo, and Institute for Computer Applications in Science and Engineering., eds. Pseudo-time method for optimal shape design using the Euler equations. Hampton, VA: Institute for Computer Applications in Science and Engineering, NASA Langley Research Center, 1995.

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35

Geojoe, Kuruvila, Ta'asan Shlomo, and Institute for Computer Applications in Science and Engineering., eds. Pseudo-time method for optimal shape design using the Euler equations. Hampton, VA: Institute for Computer Applications in Science and Engineering, NASA Langley Research Center, 1995.

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36

L, Ashby Dale, and Ames Research Center, eds. Study of the integration of wind tunnel and computational methods for aerodynamic configurations. Moffett Field, Calif: National Aeronautics and Space Administration, Ames Research Center, 1989.

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37

United States. National Aeronautics and Space Administration., ed. Flow simulations about steady-complex and unsteady moving configurations using structured-overlapped and unstructured grids: Abstract. [Washington, D.C: National Aeronautics and Space Administration, 1995.

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38

United States. National Aeronautics and Space Administration., ed. Implementation of a multiblock sensitivity analysis method in numerical aerodynamic shape optimization: Abstract. [Washington, D.C: National Aeronautics and Space Administration, 1995.

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39

D, Thomas Scott, Cliff Susan E, and Research Institute for Advanced Computer Science (U.S.), eds. An edge-based solution-adaptive method applied to the AIRPLANE code. [Moffett Field, CA]: Research Institute for Advanced Computer Science, NASA Ames Research Center, 1995.

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40

D, Thomas Scott, Cliff Susan E, and Research Institute for Advanced Computer Science (U.S.), eds. An edge-based solution-adaptive method applied to the AIRPLANE code. [Moffett Field, CA]: Research Institute for Advanced Computer Science, NASA Ames Research Center, 1995.

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41

Z, Pirzadeh Shahyar, and Langley Research Center, eds. Tetrahedral finite-volume solutions to the Navier-Stokes equations on complex configurations. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1998.

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42

Z, Pirzadeh Shahyar, and Langley Research Center, eds. Tetrahedral finite-volume solutions to the Navier-Stokes equations on complex configurations. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1998.

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43

Z, Pirzadeh Shahyar, and Langley Research Center, eds. Tetrahedral finite-volume solutions to the Navier-Stokes equations on complex configurations. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1998.

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44

Z, Pirzadeh Shahyar, and Langley Research Center, eds. Tetrahedral finite-volume solutions to the Navier-Stokes equations on complex configurations. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1998.

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45

1951-, Magnus Alfred, ed. PAN AIR-a computer program for predicting subsonic or supersonic linear potential flows about arbitrary configurations using a higher order panel method. [Moffett Field, Calif.]: NASA Ames Research Center, 1990.

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46

W, Sidwell Kenneth, ed. PAN AIR-a computer program for predicting subsonic or supersonic linear potential flows about arbitrary configurations using a higher order panel method. [Moffett Field, Calif.]: NASA Ames Research Center, 1990.

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47

W, Sidwell Kenneth, ed. PAN AIR-a computer program for predicting subsonic or supersonic linear potential flows about arbitrary configurations using a higher order panel method. [Moffett Field, Calif.]: NASA Ames Research Center, 1990.

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48

PAN AIR-a computer program for predicting subsonic or supersonic linear potential flows about arbitrary configurations using a higher order panel method. [Moffett Field, Calif.]: NASA Ames Research Center, 1990.

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49

PAN AIR-a computer program for predicting subsonic or supersonic linear potential flows about arbitrary configurations using a higher order panel method. [Moffett Field, Calif.]: NASA Ames Research Center, 1990.

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50

1951-, Magnus Alfred, ed. PAN AIR-a computer program for predicting subsonic or supersonic linear potential flows about arbitrary configurations using a higher order panel method. [Moffett Field, Calif.]: NASA Ames Research Center, 1990.

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