Synopsis
《标准驱动：基于标准的美国基础教育改革》是关于美国标准驱动的教育改革的系统研究之作，不仅研究了改革的产生缘由、内涵及进程，而且从标准、课程、教学、评价绩效责任和教师教育六大方面对改革涉及的内容进行了深入研究。在分析各主要内容时，力求做到全面，即系统地把握其特点、现状、问题与趋势；力求做到深入，即在整体上把握多样化的州策略的差异性和共性的同时，撷取若干个案进行深入研究与分析。在研究标准、课程等内容时，力求做到静态分析和动态研究相结合。所谓静态分析就是把握研究对象现时态的特征，如在研究美国标准时，分析了多样化的标准文本的特征；所谓动态研究就是要考察研究对象的产生、发展变化的过程，如在研究标准时，分析了这些标准的研制过程。静态分析和动态研究的结合有助于全面把握研究对象。
《标准驱动：基于标准的美国基础教育改革》还是中美基础教育改革的比较研究之作，例如，在《标准驱动：基于标准的美国基础教育改革》的最后一章，从不同的角度对中美两国的基础教育改革进行系统地比较，在比较的基础上，对我国当前基础教育改革中的若干问题进行了思考并提出了若干建议。具体说来，《标准驱动：基于标准的美国基础教育改革》共分为三个部分八个章节。
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aeroelastic design basis (2nd edition)
Edité par
Beijing Aerospace University Press Pub. Date :2010, 2010
ISBN 10 : 7811249391
ISBN 13 : 9787811249392
Neuf
paperback
Vendeur : liu xing, Nanjing, JS, Chine
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paperback. Etat : New. Ship out in 2 business day, And Fast shipping, Free Tracking number will be provided after the shipment.Pages Number: 203 Publisher: Beijing Aerospace University Press Pub. Date :2010-01 This book describes the aerodynamic design of the basic principles of flexibility and the basic methods. including 4 parts: the static aeroelastic problem. aeroelastic dynamic stability - flutter. aeroservoelastic aeroelastic stability analysis and testing. Addition to describing the basic concepts and theories. the book also describes the commonly used engineering approach; aeroelastic technology in recent years new developments. but also gave a brief introduction. This book can serve as institutions of higher aviation-related undergraduate and graduate teaching books or reference books are also available for the aviation industry and other industrial sectors design officers. Contents: Chapter 1 Introduction 1.1 Overview 1.2 aeroelastic aeroelastic problem of the mechanical outline of the historical development of aero-elastic block diagram 1.3 1.4 1.5 Classification of aeroelastic problems in aircraft design in the aeroelastic design 1.6 aeroelastic design in new developments in aircraft design thinking questions References Chapter 2 aeroelastic static problem the basic principles and analytical methods 2.1 aeroelastic static problem of the basic principles of long straight wing 2.2 Analytical methods thinking questions References Chapter 3 Static aeroelastic analysis of the problem matrix 3.1 aerodynamic influence coefficient matrix 3.2 Static Aeroelastic Analysis of basic equations 3.3 3.4 Calculation and analysis of divergent wing wing load calculation and analysis of the redistribution of 3.5 aileron control efficiency and counter-thinking questions References 4 Chapter unsteady aerodynamic calculations 4.1 4.2 Non-quasi-steady aerodynamic setFour Satisfaction guaranteed,or money back. N° de réf. du vendeur J54242
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