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  • General Aviation Aircraft Load Analysis

    General Aviation Aircraft Load Analysis by Gudmundsson, Snorri;

      • GET 10% OFF

      • The discount is only available for 'Alert of Favourite Topics' newsletter recipients.
      • Publisher's listprice EUR 110.00
      • The price is estimated because at the time of ordering we do not know what conversion rates will apply to HUF / product currency when the book arrives. In case HUF is weaker, the price increases slightly, in case HUF is stronger, the price goes lower slightly.

        45 622 Ft (43 450 Ft + 5% VAT)
      • Discount 10% (cc. 4 562 Ft off)
      • Discounted price 41 060 Ft (39 105 Ft + 5% VAT)

    45 622 Ft

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    Product details:

    • Publisher Butterworth-Heinemann
    • Date of Publication 1 January 2022

    • ISBN 9780128034859
    • Binding Paperback
    • No. of pages416 pages
    • Size 235x191 mm
    • Language English
    • 0

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    Long description:

    General Aviation Aircraft Load Analysis provides new detail to benefit those studying and working in general aviation aircraft structural design. Load analysis is an indispensable preliminary element of aircraft structural design, defining aerodynamic, inertial and operational loads to which the airframe must be equipped to react. Snorri Gudmundsson (author of General Aviation Aircraft Design) provides a clear and practical study of load analysis for general aviation aircraft-the first book to do so. The book explains basic concepts like aerodynamic and inertial loads, as well as new practical methods for calculation including numerical and experimental analyses.




    • Focuses exclusively on load for GA aircraft
    • Balances basic concepts of load estimation and practical methods of load calculation
    • Addresses load estimation using both numerical and experimental methods
    • Provides a clear and practical study of load analysis for general aviation aircraft - the first book to do so

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    Table of Contents:

    1. Introduction 2. Fundamentals of Aircraft Structures 3. Planar and Volumetric Properties 4. Aircraft Weight and Balance 5. Fundamentals of Kinematics, Statics, and Dynamics 6. Fundamentals of Statics 7. Shear, Moment, and Torsion Diagrams 8. Fundamentals of Mechanics of Materials 9. Structural Load Analysis 10. The Flight Envelope 11. Inertial Loads 12. Aerodynamic Loads - Classical Methods 13. Aerodynamic Loads - Numerical Methods 14. Control System Loads 15. Operational Loads 16. Selected Compliance Methods

    Appendix A - Miscellaneous Information Appendix B - Solutions of Second Order Ordinary Differential Equations

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