Isbn: 9783847302353 - design of solar powered high altitude long endurance unmanned biplanes: a preliminary study (6 risultati)

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  • Lingua: Inglese

    Editore: LAP LAMBERT Academic Publishing, 2011

    3847302353 / 9783847302353

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    Da: Mispah books, Redhill, SURRE, Regno UnitoMispah books

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    Condizione: Usato - Come nuovo

    EUR 177,66

    EUR 29,54 spedizione 
    Spedito da Regno Unito a U.S.A.

    Quantità: 1 disponibile

    Paperback. Condizione: Like New. LIKE NEW. SHIPS FROM MULTIPLE LOCATIONS. book.

  • Lingua: Inglese

    Editore: LAP LAMBERT Academic Publishing Dez 2011, 2011

    3847302353 / 9783847302353

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    Da: BuchWeltWeit Ludwig Meier e.K., Bergisch Gladbach, GermaniaBuchWeltWeit Ludwig Meier e.K.

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    EUR 79,00

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    Taschenbuch. Condizione: Neu. This item is printed on demand - it takes 3-4 days longer - Neuware -In the last few years, the interest regarding solar powered aircraft has increased significantly and, in particular, the attention has been focused on Unmanned Aerial Vehicles (UAV), able to perform High Altitude and Long Endurance (HALE) missions for telecommunication, remote sensing, surveillance and control, both for civil and military applications. The present book shows the results of a research about Solar Powered Biplanes (SPBs), dealing with the definition of a design methodology and the introduction of new design tools for this kind of aircraft. The potential benefits of choosing a biplane architecture are explained and mission requirements are introduced in order to define two types of mission, conceived to perform the two main tasks of such kind of UAVs: Telecommunication (TLC) and Intelligence, Reconnaissance and Surveillance (IRS) operations. The design procedure is illustrated and a method for the preliminary aircraft sizing, based on design curves, is proposed. The optimization method adopted for the UAV design is presented, together with the models used to study aerodynamics, flight mechanics, energy balance, structures and propulsion systems. 320 pp. Englisch.…

  • Lingua: Inglese

    Editore: LAP LAMBERT Academic Publishing, 2011

    3847302353 / 9783847302353

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    Da: moluna, Greven, Germaniamoluna

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    EUR 63,42

    EUR 48,99 spedizione 
    Spedito da Germania a U.S.A.

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    Condizione: New. Dieser Artikel ist ein Print on Demand Artikel und wird nach Ihrer Bestellung fuer Sie gedruckt. Autor/Autorin: Cipolla VittorioVittorio Cipolla is a Postdoctoral Research Fellow at the Department of Aerospace Engineering of Pisa University (Italy), where he achieved the BSc, MSc and PhD degrees. His research activities concern the study of bo.…

  • Lingua: Inglese

    Editore: LAP LAMBERT Academic Publishing, 2011

    3847302353 / 9783847302353

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    Da: preigu, Osnabrück, Germaniapreigu

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    EUR 65,80

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    Taschenbuch. Condizione: Neu. Design of Solar Powered High Altitude Long Endurance Unmanned Biplanes | A preliminary study | Vittorio Cipolla | Taschenbuch | 320 S. | Englisch | 2011 | LAP LAMBERT Academic Publishing | EAN 9783847302353 | Verantwortliche Person für die EU: preigu GmbH & Co. KG, Lengericher Landstr. 19, 49078 Osnabrück, mail[at]preigu[dot]de | Anbieter: preigu Print on Demand. …

  • Lingua: Inglese

    Editore: LAP LAMBERT Academic Publishing Dez 2011, 2011

    3847302353 / 9783847302353

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    Da: buchversandmimpf2000, Emtmannsberg, BAYE, Germaniabuchversandmimpf2000

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    Condizione: Nuovo

    EUR 79,00

    EUR 60,00 spedizione 
    Spedito da Germania a U.S.A.

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    Taschenbuch. Condizione: Neu. This item is printed on demand - Print on Demand Titel. Neuware -In the last few years, the interest regarding solar powered aircraft has increased significantly and, in particular, the attention has been focused on Unmanned Aerial Vehicles (UAV), able to perform High Altitude and Long Endurance (HALE) missions for telecommunication, remote sensing, surveillance and control, both for civil and military applications. The present book shows the results of a research about Solar Powered Biplanes (SPBs), dealing with the definition of a design methodology and the introduction of new design tools for this kind of aircraft. The potential benefits of choosing a biplane architecture are explained and mission requirements are introduced in order to define two types of mission, conceived to perform the two main tasks of such kind of UAVs: Telecommunication (TLC) and Intelligence, Reconnaissance and Surveillance (IRS) operations. The design procedure is illustrated and a method for the preliminary aircraft sizing, based on design curves, is proposed. The optimization method adopted for the UAV design is presented, together with the models used to study aerodynamics, flight mechanics, energy balance, structures and propulsion systems.VDM Verlag, Dudweiler Landstraße 99, 66123 Saarbrücken 320 pp. Englisch.…

  • Lingua: Inglese

    Editore: LAP LAMBERT Academic Publishing, 2011

    3847302353 / 9783847302353

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    • Print on Demand

    Da: AHA-BUCH GmbH, Einbeck, GermaniaAHA-BUCH GmbH

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    Condizione: Nuovo

    EUR 79,00

    EUR 62,48 spedizione 
    Spedito da Germania a U.S.A.

    Quantità: 1 disponibile

    Taschenbuch. Condizione: Neu. nach der Bestellung gedruckt Neuware - Printed after ordering - In the last few years, the interest regarding solar powered aircraft has increased significantly and, in particular, the attention has been focused on Unmanned Aerial Vehicles (UAV), able to perform High Altitude and Long Endurance (HALE) missions for telecommunication, remote sensing, surveillance and control, both for civil and military applications. The present book shows the results of a research about Solar Powered Biplanes (SPBs), dealing with the definition of a design methodology and the introduction of new design tools for this kind of aircraft. The potential benefits of choosing a biplane architecture are explained and mission requirements are introduced in order to define two types of mission, conceived to perform the two main tasks of such kind of UAVs: Telecommunication (TLC) and Intelligence, Reconnaissance and Surveillance (IRS) operations. The design procedure is illustrated and a method for the preliminary aircraft sizing, based on design curves, is proposed. The optimization method adopted for the UAV design is presented, together with the models used to study aerodynamics, flight mechanics, energy balance, structures and propulsion systems.…