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  • 1
    ISSN: 1520-4995
    Source: ACS Legacy Archives
    Topics: Biology , Chemistry and Pharmacology
    Type of Medium: Electronic Resource
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  • 2
    Electronic Resource
    Electronic Resource
    Bingley : Emerald
    Aircraft engineering and aerospace technology 72 (2000), S. 334-344 
    ISSN: 0002-2667
    Source: Emerald Fulltext Archive Database 1994-2005
    Topics: Mechanical Engineering, Materials Science, Production Engineering, Mining and Metallurgy, Traffic Engineering, Precision Mechanics
    Notes: So far the literature on inverse shape design in aerodynamics is still confined to the single-point (nominal design point) design and to steady flow. This situation cannot cope with the modern development of internal and external aerodynamics and aerothermoelasticity, especially turbomachinery and aircraft flows. Accordingly, in recent years a new generation of inverse shape design problem has been suggested and investigated theoretically and computationally, consisting mainly of: unsteady inverse and hybrid problems; multipoint inverse and hybrid problems; and inverse problem in aerothermoelasticity. It opens a new area of research in fluid mechanics and aerothermoelasticity. An overview of its status and perspective is given herein, emphasizing the new concepts, theory and methods of solution involved.
    Type of Medium: Electronic Resource
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  • 3
    Electronic Resource
    Electronic Resource
    Bingley : Emerald
    Aircraft engineering and aerospace technology 76 (2004), S. 516-522 
    ISSN: 0002-2667
    Source: Emerald Fulltext Archive Database 1994-2005
    Topics: Mechanical Engineering, Materials Science, Production Engineering, Mining and Metallurgy, Traffic Engineering, Precision Mechanics
    Notes: As a kind of free (unknown) boundary problems, inverse shape design of airfoils attracts extensive attention in recent years. By variable-domain variational theory, free boundary condition can be coupled with the governing equations for flow field, which makes it possible to calculate the flow field with the free boundary simultaneously. In this paper, the variational principle (VP) of 2D airfoil shape design problem is obtained from the basic dimensionless velocity potential equations for 2D compressible flow by using systematic approach and variable-domain variational formula. The deformable finite element method based on the VP is used to segmentally design airfoil at two design points (angles of attack) and four design points, respectively. The results show that the present method is highly effective and accurate to solve multipoint inverse problem of airfoils.
    Type of Medium: Electronic Resource
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  • 4
    Electronic Resource
    Electronic Resource
    Bingley : Emerald
    Aircraft engineering and aerospace technology 69 (1997), S. 527-533 
    ISSN: 0002-2667
    Source: Emerald Fulltext Archive Database 1994-2005
    Topics: Mechanical Engineering, Materials Science, Production Engineering, Mining and Metallurgy, Traffic Engineering, Precision Mechanics
    Notes: Presents a brief overview of some new concepts and research results concerning aerodynamic computation and design of jet-propulsion engines with emphasis on turbomachinery (TM) developed in China, without any attempt to be exhaustive.
    Type of Medium: Electronic Resource
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  • 5
    Electronic Resource
    Electronic Resource
    Bingley : Emerald
    Aircraft engineering and aerospace technology 76 (2004), S. 376-383 
    ISSN: 0002-2667
    Source: Emerald Fulltext Archive Database 1994-2005
    Topics: Mechanical Engineering, Materials Science, Production Engineering, Mining and Metallurgy, Traffic Engineering, Precision Mechanics
    Notes: As a kind of free (unknown) boundary problem, inverse shape design of airfoils has attracted extensive attention in recent years. By variable-domain variational theory, free boundary condition can be coupled with the governing equations for flow field, which makes it possible to calculate the flow field with the free boundary simultaneously. In this paper, the variational principle (VP) of 2D airfoil shape design problem is obtained from the basic dimensionless velocity potential equations for 2D compressible flow by using a systematic approach and variable-domain variational formula. The deformable finite element method based on the VP is used to segmentally design airfoil at two design points (angles of attack) and four design points, respectively. The results show that the present method is highly effective and accurate for solving multipoint inverse problem of airfoils.
    Type of Medium: Electronic Resource
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  • 6
    Electronic Resource
    Electronic Resource
    s.l. ; Stafa-Zurich, Switzerland
    Key engineering materials Vol. 368-372 (Feb. 2008), p. 18-20 
    ISSN: 1013-9826
    Source: Scientific.Net: Materials Science & Technology / Trans Tech Publications Archiv 1984-2008
    Topics: Mechanical Engineering, Materials Science, Production Engineering, Mining and Metallurgy, Traffic Engineering, Precision Mechanics
    Notes: In the frame of shock-induced depoling, PZT 95/5 ferroelectric ceramics with niobium dopedhas been assembled for the pulsed power supply, and the electrical current output has been investigatedunder the action of shock wave in a "normal mode". The electrical response of LRC load especially for thesmall resistance (R) and small inductance (L) load was studied. Plane-shock-wave tests were conducted,and the PZT 95/5 ceramics stacked in parallel were devised to generate high-power electrical pulse. Anoutput current of 7 kA has been obtained, and the corresponding rise time of the front edge is under 500ns. Theoretical calculations were conducted and a good agreement with the experiment presented
    Type of Medium: Electronic Resource
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  • 7
    Electronic Resource
    Electronic Resource
    s.l. ; Stafa-Zurich, Switzerland
    Materials science forum Vol. 532-533 (Dec. 2006), p. 1144-1147 
    ISSN: 1662-9752
    Source: Scientific.Net: Materials Science & Technology / Trans Tech Publications Archiv 1984-2008
    Topics: Mechanical Engineering, Materials Science, Production Engineering, Mining and Metallurgy, Traffic Engineering, Precision Mechanics
    Notes: This paper presents an innovative product design system based on Quality FunctionDevelopment (QFD) and Theory of Inventive Problem Solving (TRIZ in Russian abbreviation).House of Quality (HOQ) is the core of QFD. To make QFD more practical and operable for smalland medium-sized companies, a simplified model of HOQ is proposed. A set of reasoning schemefor inferring requirements relationships is adopted to facilitate constructing the HOQ. Thecontradiction in the process of mechanical design is defined by TRIZ as physical contradiction andtechnical contradiction. These two contradictions are solved through contradiction matrix andinventive principles of TRIZ. The innovative design system mainly uses the tool of contradictionmatrix to solve the bottle techniques attained from QFD. By taking the HOQ as its interface theintegration between QFD and TRIZ is realized. After conducting quality function development, twooutputs can be obtained. They are the technical measure needing improvement and the technicalmeasure that is getting worse while improving the former one. These two measures are taken asinputs of TRIZ module to analyze and solve the problem of product design
    Type of Medium: Electronic Resource
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