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[资源] 分享——飞机飓风载荷：概念与应用（英文版）

"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

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Pureland

木虫之王 (知名作家)

应助: 1516 (讲师)
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