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    "Gust Loads on Aircraft: Concepts and Applications" by Frederic M. Hoblit

    Posted By: exLib
    "Gust Loads on Aircraft: Concepts and Applications" by Frederic M. Hoblit

    "Gust Loads on Aircraft: Concepts and Applications" by Frederic M. Hoblit, consultant
    American Institute of Aeronautics and Astronautics. AIAA EDducation Series, Volume 3797
    AIAA | 1988/2001 | ISBN: 0930403452 9780930403454 | 320 pages | PDF | 17 MB

    This book provides an authoritative and practical presentation of the determination of gust loads on airplanes, especially continuous turbulence gust loads. The text emphasizes the basic concepts involved in gust load determination and enriches the material with discussion of important relationships, definitions of terminology and nomenclature, historical perspective, and explanations of relevant calculations. Coverage begins with discrete-gust idealization of the gust structure and moves to continuous-turbulence gust loads.

    Also considered are loads combination and design criteria, gust-response equations of motion, spanwise variation of vertical gust velocity, nonlinear systems, and analysis of gust-response flight-test data.

    Table of Contents
    Foreword
    Preface
    Gust Loads Fundamentals
    Discrete-Gust Static Loads
    Discrete-Gust Dynamic Loads
    Basic PSD Concepts and Application to Gust Loads
    Continuous Turbulence Gust Loads Criteria
    Load Combinations and Design Conditions
    Gust Response Equations of Motion: Formulation and Solution
    Short-Cut Methods
    Spanwise Variation of Vertical Gust Velocity
    Treatment of Nonlinear Systems
    Analysis of Gust-Response Flight-Test Data
    Adequacy of the Stationary-Gaussian Idealization of the Gust Structure
    Present Place of Discrete-Gust Load Requirements
    Plunge-Only Equation of Motion for an Airplane Encountering a One-Minus-Cosine Vertical Gust
    Elementary Introduction to Some Concepts in Probability Theory and Statistics
    Gaussian Probability Distribution Plots
    Ratio of von Karman to Dryden Gust PSD's
    Upper Limit of Integration in Computation of A, N0 and p
    Plots of σw Probability Distributions
    Derivation of Generalized Frequency of Exceedance Equation
    Relative Ultimate Gust Capabilities for Upbending, Downbending, and Lateral Gust
    Most Likely σw Value Associated with a Particular Load Level
    Matrices and Matrix Algebra
    C.G. Acceleration PSD's for an Idealized Rigid Airplane Free to Pitch and Plunge
    Annotated Bibliography
    References
    Subject Index
    with TOC BookMarkLinks