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[資源]
分享——飛機颶風載荷：概念與應用（英文版）
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"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 AIAA | 1988/2001 | ISBN: 0930403452 9780930403454 | 320 pages | PDF | 17 MB [ Last edited by Pureland on 2013-6-13 at 10:04 ] |
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