9787811249392 - 标准驱动：基于标准的美国基础教育改革 (1 risultati)
Lingua: Cinese
Editore: Beijing Aerospace University Press Pub. Date :2010, 2010
- Brossura
Da: liu xing, Nanjing, JS, Cinaliu xing
Contatta il venditoreVenditore con 5 stelleCondizione: Nuovo
EUR 49,84
EUR 15,77 spedizioneSpedito da Cina a U.S.A.Quantità: 10 disponibili
paperback. Condizione: 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.
