Isbn: 9781118568118 - advanced aircraft design: conceptual design, analysis and optimization of subsonic civil airplanes (aerospace series) (24 resultados)

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  • Idioma: Inglés

    Editorial: Wiley, 2013

    1118568117 / 9781118568118

    Serie: Libro 8 de 23 - Aerospace Series

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    Editorial: Wiley, 2013

    1118568117 / 9781118568118

    Serie: Libro 8 de 23 - Aerospace Series

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  • Idioma: Inglés

    Editorial: Wiley, 2013

    1118568117 / 9781118568118

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    Editorial: Wiley, 2013

    1118568117 / 9781118568118

    Serie: Libro 8 de 23 - Aerospace Series

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  • Idioma: Inglés

    Editorial: Wiley, 2013

    1118568117 / 9781118568118

    Serie: Libro 8 de 23 - Aerospace Series

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  • Idioma: Inglés

    Editorial: Wiley, 2013

    1118568117 / 9781118568118

    Serie: Libro 8 de 23 - Aerospace Series

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  • Idioma: Inglés

    Editorial: Wiley, 2013

    1118568117 / 9781118568118

    Serie: Libro 8 de 23 - Aerospace Series

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  • Idioma: Inglés

    Editorial: Wiley, 2013

    1118568117 / 9781118568118

    Serie: Libro 8 de 23 - Aerospace Series

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    Librería: Ria Christie Collections, Uxbridge, Reino UnidoRia Christie Collections

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    Condición: New. In English.

  • Idioma: Inglés

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    1118568117 / 9781118568118

    Serie: Libro 8 de 23 - Aerospace Series

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    Hardback. Condición: New. Although the overall appearance of modern airliners has not changed a lot since the introduction of jetliners in the 1950s, their safety, efficiency and environmental friendliness have improved considerably. Main contributors to this have been gas turbine engine technology, advanced materials, computational aerodynamics, advanced structural analysis and on-board systems. Since aircraft design became a highly multidisciplinary activity, the development of multidisciplinary optimization (MDO) has become a popular new discipline. Despite this, the application of MDO during the conceptual design phase is not yet widespread. Advanced Aircraft Design: Conceptual Design, Analysis and Optimization of Subsonic Civil Airplanes presents a quasi-analytical optimization approach based on a concise set of sizing equations. Objectives are aerodynamic efficiency, mission fuel, empty weight and maximum takeoff weight. Independent design variables studied include design cruise altitude, wing area and span and thrust or power loading. Principal  features of integrated concepts such as the blended wing and body and highly non-planar wings are also covered.  The quasi-analytical approach enables designers to compare the results of high-fidelity MDO optimization with lower-fidelity methods which need far less computational effort. Another advantage to this approach is that it can provide answers to "what if" questions rapidly and with little computational cost. Key features: Presents a new fundamental vision on conceptual airplane design optimizationProvides an overview of advanced technologies for propulsion and reducing aerodynamic dragOffers insight into the derivation of design sensitivity informationEmphasizes design based on first principlesConsiders pros and cons  of innovative configurationsReconsiders optimum cruise performance at transonic Mach numbers Advanced Aircraft Design: Conceptual Design, Analysis and Optimization of Subsonic Civil Airplanes advances understanding of the initial optimization of civil airplanes and is a must-have reference for aerospace engineering students, applied researchers, aircraft design engineers and analysts. …

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    Editorial: John Wiley & Sons Inc, 2013

    1118568117 / 9781118568118

    Serie: Libro 8 de 23 - Aerospace Series

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    Condición: New. Although the overall appearance of modern airliners has not changed a lot since the introduction of jetliners in the 1950s, their safety, efficiency and environmental friendliness have improved considerably. Series: Aerospace Series. Num Pages: 436 pages, black & white illustrations, black & white tables, figures. BIC Classification: TRP. Category: (P) Professional & Vocational. Dimension: 252 x 172 x 28. Weight in Grams: 898. . 2013. 1st Edition. Hardcover. . . . . …

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    Condición: New. pp. 440.

  • Idioma: Inglés

    Editorial: Wiley, 2013

    1118568117 / 9781118568118

    Serie: Libro 8 de 23 - Aerospace Series

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    Editorial: John Wiley & Sons, 2013

    1118568117 / 9781118568118

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    Condición: New. pp. 440 Index.

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    Condición: New. Advanced Aircraft Design: Conceptual Design, Analysis and Optimization of Subsonic Civil Airplanes advances understanding of the initial optimization of civil airplanes and is a must-have reference for aerospace engineering students, applied researchers, a.

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    Editorial: John Wiley & Sons Inc, 2013

    1118568117 / 9781118568118

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    Condición: New. Although the overall appearance of modern airliners has not changed a lot since the introduction of jetliners in the 1950s, their safety, efficiency and environmental friendliness have improved considerably. Series: Aerospace Series. Num Pages: 436 pages, black & white illustrations, black & white tables, figures. BIC Classification: TRP. Category: (P) Professional & Vocational. Dimension: 252 x 172 x 28. Weight in Grams: 898. . 2013. 1st Edition. Hardcover. . . . . Books ship from the US and Ireland. …

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    Hardcover. Condición: Brand New. 3rd edition. 432 pages. 9.84x6.85x0.87 inches. In Stock.

  • Idioma: Inglés

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    1118568117 / 9781118568118

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    Hardback. Condición: New. Although the overall appearance of modern airliners has not changed a lot since the introduction of jetliners in the 1950s, their safety, efficiency and environmental friendliness have improved considerably. Main contributors to this have been gas turbine engine technology, advanced materials, computational aerodynamics, advanced structural analysis and on-board systems. Since aircraft design became a highly multidisciplinary activity, the development of multidisciplinary optimization (MDO) has become a popular new discipline. Despite this, the application of MDO during the conceptual design phase is not yet widespread. Advanced Aircraft Design: Conceptual Design, Analysis and Optimization of Subsonic Civil Airplanes presents a quasi-analytical optimization approach based on a concise set of sizing equations. Objectives are aerodynamic efficiency, mission fuel, empty weight and maximum takeoff weight. Independent design variables studied include design cruise altitude, wing area and span and thrust or power loading. Principal  features of integrated concepts such as the blended wing and body and highly non-planar wings are also covered.  The quasi-analytical approach enables designers to compare the results of high-fidelity MDO optimization with lower-fidelity methods which need far less computational effort. Another advantage to this approach is that it can provide answers to "what if" questions rapidly and with little computational cost. Key features: Presents a new fundamental vision on conceptual airplane design optimizationProvides an overview of advanced technologies for propulsion and reducing aerodynamic dragOffers insight into the derivation of design sensitivity informationEmphasizes design based on first principlesConsiders pros and cons  of innovative configurationsReconsiders optimum cruise performance at transonic Mach numbers Advanced Aircraft Design: Conceptual Design, Analysis and Optimization of Subsonic Civil Airplanes advances understanding of the initial optimization of civil airplanes and is a must-have reference for aerospace engineering students, applied researchers, aircraft design engineers and analysts. …

  • Idioma: Inglés

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    Editorial: John Wiley & Sons Inc, New York, 2013

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    Hardcover. Condición: new. Hardcover. Although the overall appearance of modern airliners has not changed a lot since the introduction of jetliners in the 1950s, their safety, efficiency and environmental friendliness have improved considerably. Main contributors to this have been gas turbine engine technology, advanced materials, computational aerodynamics, advanced structural analysis and on-board systems. Since aircraft design became a highly multidisciplinary activity, the development of multidisciplinary optimization (MDO) has become a popular new discipline. Despite this, the application of MDO during the conceptual design phase is not yet widespread. Advanced Aircraft Design: Conceptual Design, Analysis and Optimization of Subsonic Civil Airplanes presents a quasi-analytical optimization approach based on a concise set of sizing equations. Objectives are aerodynamic efficiency, mission fuel, empty weight and maximum takeoff weight. Independent design variables studied include design cruise altitude, wing area and span and thrust or power loading. Principal features of integrated concepts such as the blended wing and body and highly non-planar wings are also covered. The quasi-analytical approach enables designers to compare the results of high-fidelity MDO optimization with lower-fidelity methods which need far less computational effort. Another advantage to this approach is that it can provide answers to what if questions rapidly and with little computational cost. Key features: Presents a new fundamental vision on conceptual airplane design optimizationProvides an overview of advanced technologies for propulsion and reducing aerodynamic dragOffers insight into the derivation of design sensitivity informationEmphasizes design based on first principlesConsiders pros and cons of innovative configurationsReconsiders optimum cruise performance at transonic Mach numbers Advanced Aircraft Design: Conceptual Design, Analysis and Optimization of Subsonic Civil Airplanes advances understanding of the initial optimization of civil airplanes and is a must-have reference for aerospace engineering students, applied researchers, aircraft design engineers and analysts. Although the overall appearance of modern airliners has not changed a lot since the introduction of jetliners in the 1950s, their safety, efficiency and environmental friendliness have improved considerably. This item is printed on demand. Shipping may be from multiple locations in the US or from the UK, depending on stock availability.…

  • Idioma: Inglés

    Editorial: John Wiley & Sons Inc, New York, 2013

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    Hardcover. Condición: new. Hardcover. Although the overall appearance of modern airliners has not changed a lot since the introduction of jetliners in the 1950s, their safety, efficiency and environmental friendliness have improved considerably. Main contributors to this have been gas turbine engine technology, advanced materials, computational aerodynamics, advanced structural analysis and on-board systems. Since aircraft design became a highly multidisciplinary activity, the development of multidisciplinary optimization (MDO) has become a popular new discipline. Despite this, the application of MDO during the conceptual design phase is not yet widespread. Advanced Aircraft Design: Conceptual Design, Analysis and Optimization of Subsonic Civil Airplanes presents a quasi-analytical optimization approach based on a concise set of sizing equations. Objectives are aerodynamic efficiency, mission fuel, empty weight and maximum takeoff weight. Independent design variables studied include design cruise altitude, wing area and span and thrust or power loading. Principal features of integrated concepts such as the blended wing and body and highly non-planar wings are also covered. The quasi-analytical approach enables designers to compare the results of high-fidelity MDO optimization with lower-fidelity methods which need far less computational effort. Another advantage to this approach is that it can provide answers to what if questions rapidly and with little computational cost. Key features: Presents a new fundamental vision on conceptual airplane design optimizationProvides an overview of advanced technologies for propulsion and reducing aerodynamic dragOffers insight into the derivation of design sensitivity informationEmphasizes design based on first principlesConsiders pros and cons of innovative configurationsReconsiders optimum cruise performance at transonic Mach numbers Advanced Aircraft Design: Conceptual Design, Analysis and Optimization of Subsonic Civil Airplanes advances understanding of the initial optimization of civil airplanes and is a must-have reference for aerospace engineering students, applied researchers, aircraft design engineers and analysts. Although the overall appearance of modern airliners has not changed a lot since the introduction of jetliners in the 1950s, their safety, efficiency and environmental friendliness have improved considerably. This item is printed on demand. Shipping may be from our UK warehouse or from our Australian or US warehouses, depending on stock availability.…

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    Hardcover. Condición: Brand New. 3rd edition. 432 pages. 9.84x6.85x0.87 inches. In Stock. This item is printed on demand.

  • Idioma: Inglés

    Editorial: John Wiley & Sons Inc, New York, 2013

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    Hardcover. Condición: new. Hardcover. Although the overall appearance of modern airliners has not changed a lot since the introduction of jetliners in the 1950s, their safety, efficiency and environmental friendliness have improved considerably. Main contributors to this have been gas turbine engine technology, advanced materials, computational aerodynamics, advanced structural analysis and on-board systems. Since aircraft design became a highly multidisciplinary activity, the development of multidisciplinary optimization (MDO) has become a popular new discipline. Despite this, the application of MDO during the conceptual design phase is not yet widespread. Advanced Aircraft Design: Conceptual Design, Analysis and Optimization of Subsonic Civil Airplanes presents a quasi-analytical optimization approach based on a concise set of sizing equations. Objectives are aerodynamic efficiency, mission fuel, empty weight and maximum takeoff weight. Independent design variables studied include design cruise altitude, wing area and span and thrust or power loading. Principal features of integrated concepts such as the blended wing and body and highly non-planar wings are also covered. The quasi-analytical approach enables designers to compare the results of high-fidelity MDO optimization with lower-fidelity methods which need far less computational effort. Another advantage to this approach is that it can provide answers to what if questions rapidly and with little computational cost. Key features: Presents a new fundamental vision on conceptual airplane design optimizationProvides an overview of advanced technologies for propulsion and reducing aerodynamic dragOffers insight into the derivation of design sensitivity informationEmphasizes design based on first principlesConsiders pros and cons of innovative configurationsReconsiders optimum cruise performance at transonic Mach numbers Advanced Aircraft Design: Conceptual Design, Analysis and Optimization of Subsonic Civil Airplanes advances understanding of the initial optimization of civil airplanes and is a must-have reference for aerospace engineering students, applied researchers, aircraft design engineers and analysts. Although the overall appearance of modern airliners has not changed a lot since the introduction of jetliners in the 1950s, their safety, efficiency and environmental friendliness have improved considerably. This item is printed on demand. Shipping may be from our Sydney, NSW warehouse or from our UK or US warehouse, depending on stock availability.…

  • Idioma: Inglés

    Editorial: John Wiley & Sons, 2013

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    Condición: New. PRINT ON DEMAND pp. 440, Abbreviations Acknowledgements.