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1

United States. National Aeronautics and Space Administration., red. Simplified, inverse, ejector design tool. [Washington, DC]: National Aeronautics and Space Administration, 1993.

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2

Takewaki, Izuru. Dynamic structural design: Inverse problem approach. Southampton: WIT Press, 2000.

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3

United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch., red. Lewis inverse design code (LINDES): Users manual. [Washington, D.C.]: National Aeronautics and Space Administration, Scientific and Technical Information Branch, 1987.

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4

Fujii, Kozo. Recent Development of Aerodynamic Design Methodologies: Inverse Design and Optimization. Wiesbaden: Vieweg+Teubner Verlag, 1999.

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5

Comi, Claudio Umberto. In prospettiva inversa: Riflessioni sulla contemporaneità. Santarcangelo di Romagna (RN): Maggioli editore, 2018.

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6

Zhang, Kunyuan. Hypersonic Curved Compression Inlet and Its Inverse Design. Singapore: Springer Singapore, 2020. http://dx.doi.org/10.1007/978-981-15-0727-4.

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7

Development, North Atlantic Treaty Organization Advisory Group for Aerospace Research and. Computational methods for aerodynamic design (inverse) and optimization. Neuilly-sur-Seine: AGARD, 1990.

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8

Neittaanmäki, P. Inverse problems and optimal design in electricity and magnetism. Oxford [England]: Clarendon Press, 1996.

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9

den, Braembussche R. van, Manna M i Von Karman Institute for Fluid Dynamics., red. Inverse design and optimisation methods: April 21-25, 1997. Rhode St. Genèse, Belgium: Von Karman Institute for Fluid Dynamics, 1997.

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10

North Atlantic Treaty Organization. Advisory Group for Aerospace Research and Development. Inverse methods for airfoil design for aeronatuical and turbomachinery applications. Neuilly sur Seine, France: AGARD, 1990.

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11

Engl, Heinz W., i Joyce McLaughlin, red. Proceedings of the Conference Inverse Problems and Optimal Design in Industry. Wiesbaden: Vieweg+Teubner Verlag, 1994. http://dx.doi.org/10.1007/978-3-322-96658-2.

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12

Piiroinen, Petteri. Statistical measurements, experiments and applications. Helsinki: Suomalainen Tiedeakatemia, 2005.

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13

Development, North Atlantic Treaty Organization Advisory Group for Aerospace Research and. Special course on inverse methods for airfoil design for aeronautical and turbomachinery applications. Neuilly-sur-Seine: AGARD, 1990.

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14

Biegler, Lorenz T. Large-Scale Optimization with Applications: Part I: Optimization in Inverse Problems and Design. New York, NY: Springer New York, 1997.

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15

International Symposium on Environmentally Conscious Design and Inverse Manufacturing (2nd 2001 Tokyo, Japan). Proceedings: Second International Symposium on Environmentally Conscious Design and Inverse Manufacturing : December 11-15, 2001, Tokyo, Japan. Los Alamitos, Calif: IEEE Computer Society, 2001.

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16

K, Pischel, Hubler D i United States. National Aeronautics and Space Administration., red. The engine design engine: A clustered computer platform for the aerodynamic inverse design and analysis of a full engine. [Washington, DC: National Aeronautics and Space Administration, 1992.

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17

Sanz, J. L. C. The engine design engine: A clustered computer platform for the aerodynamic inverse design and analysis of a full engine. [Washington, DC: National Aeronautics and Space Administration, 1992.

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18

International Symposium on Environmentally Conscious Design and Inverse Manufacturing (3rd 2003 Tokyo, Japan). 2003 3rd International Symposium on Environmentally Conscious Design and Inverse Manufacturing--EcoDesign '03 : December 8-11, 2003, Tokyo, Japan. Piscataway, N.J: IEEE, 2003.

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19

Taurisson, Alain. Pédagogie de l'activité: Pour une nouvelle classe inversée : théorie et pratique du "travail d'apprendre". Issy-les-Moulineaux: Esf éditeur, 2015.

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20

W, Engl Heinz, i McLaughlin Joyce, red. Proceedings of the conference "Inverse problems and optimal design in industry": July 8-10, 1993, Philadelphia, Pa., USA. Stuttgart: B.G. Teubner, 1994.

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21

United States. National Aeronautics and Space Administration., red. Development of direct-inverse 3-D method for applied aerodynamic design and analysis: Semiannual progress report, July 1, 1986 - December 31, 1986. College Station, Tex: Texas Engineering Experiment Station, Aerospace Engineering Department, Texas A&M University, 1987.

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22

United States. National Aeronautics and Space Administration., red. Development of direct-inverse 3-D method for applied aerodynamic design and analysis: Semiannual progress report, July 1, 1986 - December 31, 1986. College Station, Tex: Texas Engineering Experiment Station, Aerospace Engineering Department, Texas A&M University, 1987.

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23

Chung, W. W. A direct application of the non-linear inverse transformation flight control system design on a STOVL aircraft. Moffett Field, Calif: National Aeronautics and Space Administration, Ames Research Center, 1993.

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24

United States. National Aeronautics and Space Administration., red. Development of direct-inverse 3-D methods for applied transonic aerodynamic wing design and analysis: Final report. College Station, Tex: Texas Engineering Experiment Station, Aerospace Engineering Department, Texas A&M University, 1990.

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25

International Symposium on Environmentally Conscious Design and Inverse Manufacturing (4th 2005 Tokyo, Japan). Proceedings: Fourth International Symposium on Environmentally Conscious Design and Inverse Manufacturing : December 12-14, 2005, Tokyo, Japan. Tokyo: Union of EcoDesigners, 2005.

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26

E, McNeill W., Stortz Michael W i Ames Research Center, red. A direct application of the non-linear inverse transformation flight control system design on a STOVL aircraft. Moffett Field, Calif: National Aeronautics and Space Administration, Ames Research Center, 1993.

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27

United States. National Aeronautics and Space Administration., red. Development of direct-inverse 3-D methods for applied transonic aerodynamic wing design and analysis: Final report. College Station, Tex: Texas Engineering Experiment Station, Aerospace Engineering Department, Texas A&M University, 1990.

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28

1933-, Yoshikawa H., Inverse Manufacturing Forum Japan, Japan Environment Management Association for Industry. i IEEE Computer Society. Technical Committee on Electronics and the Environment., red. Proceedings: First International Symposium on Environmentally Conscious Design and Inverse Manufacturing : February 1-3, 1999, Tokyo, Japan. Los Alamitos, California: IEEE Computer Society, 1999.

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29

North Atlantic Treaty Organization. Advisory Group for Aerospace Research and Development. Technical evaluation report on the Fluid Dynamics Panel Symposium on computational methods for aerodynamic design (inverse) and optimization. Neuilly-sur-Seine: AGARD, 1990.

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30

Nelson, P. A. MINT, the multiple error LMS algorithm, and the design of inverse filters for multi-channel sound reproduction systems. Southampton, England: University of Southampton, 1992.

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31

United States. National Aeronautics and Space Administration., red. Development of direct-inverse 3-D methods for applied aerodynamic design and analysis: Semiannual progress report, July 1, 1987 - December 31, 1987. College Station, Tex: Texas Engineering Experiment Station, Aerospace Engineering Department, Texas A&M University, 1988.

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32

United States. National Aeronautics and Space Administration., red. Development of direct-inverse 3-D methods for applied aerodynamic design and analysis: Semiannual progress report, July 1, 1987 - December 31, 1987. College Station, Tex: Texas Engineering Experiment Station, Aerospace Engineering Department, Texas A&M University, 1988.

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33

United States. National Aeronautics and Space Administration, red. Development of direct-inverse 3-D methods for applied aerodynamic design and analysis: Semiannual progress report, July 1, 1987 - December 31, 1987. College Station, Tex: Texas Engineering Experiment Station, Aerospace Engineering Department, Texas A&M University, 1988.

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34

United States. National Aeronautics and Space Administration, red. Development of direct-inverse 3-D method for applied aerodynamic design and analysis: Semiannual progress report, July 1, 1986 - December 31, 1986. College Station, Tex: Texas Engineering Experiment Station, Aerospace Engineering Department, Texas A&M University, 1987.

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35

United States. National Aeronautics and Space Administration, red. Development of direct-inverse 3-D methods for applied aerodynamic design and analysis: Semiannual progress report, July 1, 1987 - December 31, 1987. College Station, Tex: Texas Engineering Experiment Station, Aerospace Engineering Department, Texas A&M University, 1988.

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36

Lavrentʹev, M. M. Computer modelling in tomography and ill-posed problemsovosibirsk, Russia, August 10-14, 1993 : abstracts. Utrecht: VSP, 2001.

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37

Biegler, Lorenz T. Large-Scale Optimization with Applications: Part III: Molecular Structure and Optimization. New York, NY: Springer New York, 1997.

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38

United States. National Aeronautics and Space Administration., red. Development of direct-inverse 3-D methods for applied transonic aerodynamic wing design and analysis: Semiannual progress report, July 1, 1988 - December 31, 1988. College Station, Tex: Texas Engineering Experiment Station, 1988.

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39

United States. National Aeronautics and Space Administration., red. Development of direct-inverse 3-D methods for applied transonic aerodynamic wing design and analysis: Semiannual progress report, January 1, 1987 - June 30, 1987. College Station, Tex: Texas Engineering Experiment Station, 1987.

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40

United States. National Aeronautics and Space Administration., red. Development of direct-inverse 3-D methods for applied transonic aerodynamic wing design and analysis: Semiannual progress report, January 1, 1987 - June 30, 1987. College Station, Tex: Texas Engineering Experiment Station, 1987.

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41

United States. National Aeronautics and Space Administration., red. Development of direct-inverse 3-D methods for applied transonic aerodynamic wing design and analysis: Semiannual progress report, July 1, 1988 - December 31, 1988. College Station, Tex: Texas Engineering Experiment Station, 1988.

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42

United States. National Aeronautics and Space Administration., red. Development of direct-inverse 3-D methods for applied transonic aerodynamic wing design and analysis: Semiannual progress report, January 1, 1988 - June 30, 1988. College Station, Tex: Texas Engineering Experiment Station, 1988.

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43

Research), International Roxie Users Meeting and Workshop (1st 1998 European Organization for Nuclear. ROXIE: Routine for the optimization of magnet X-sections, inverse field calculation and coil end design : First International Roxie Users Meeting and Workshop, CERN, 16-18 March 1998, proceedings. Geneva: CERN, European Organization for Nuclear Research, 1999.

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44

Simplified, inverse, ejector design tool. [Washington, DC]: National Aeronautics and Space Administration, 1993.

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45

National Aeronautics and Space Administration (NASA) Staff. Simplified, Inverse, Ejector Design Tool. Independently Published, 2018.

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46

Lewis inverse design code (LINDES): Users manual. [Washington, D.C.]: National Aeronautics and Space Administration, Scientific and Technical Information Branch, 1987.

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47

Chen, Qingyan, Tengfei Zhang, Xueyi You i Zhiqiang Zhai. Inverse Design Methods for the Built Environment. CRC Press LLC, 2017.

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48

Chen, Qingyan, Zhiqiang Zhai, Xueyi You i Tengfei Zhang. Inverse Design Methods for the Built Environment. Routledge, 2017. http://dx.doi.org/10.4324/9781315468013.

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49

Chen, Qingyan, Tengfei Zhang, Xueyi You i Zhiqiang Zhai. Inverse Design Methods for the Built Environment. CRC Press LLC, 2017.

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50

Chen, Qingyan, Tengfei Zhang, Xueyi You i Zhiqiang Zhai. Inverse Design Methods for the Built Environment. CRC Press LLC, 2017.

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