1# Library to Find Best eBook for Read
Author : Wahyu Hendriyono
Release : 2000
Genre : Aerodynamic load
Kind : eBook
Book Rating : /5 ( reviews)
Book Synopsis Aerodynamic Load Estimation of a Manoeuvring Aircraft by : Wahyu Hendriyono
Download or read book Aerodynamic Load Estimation of a Manoeuvring Aircraft written by Wahyu Hendriyono. This book was released on 2000. Available in PDF, EPUB and Kindle. Book excerpt:
Author : Jan R. Wright
Release : 2014-12-16
Genre : Technology & Engineering
Kind : eBook
Book Rating : 422/5 ( reviews)
Book Synopsis Introduction to Aircraft Aeroelasticity and Loads by : Jan R. Wright
Download or read book Introduction to Aircraft Aeroelasticity and Loads written by Jan R. Wright. This book was released on 2014-12-16. Available in PDF, EPUB and Kindle. Book excerpt: Introduction to Aircraft Aeroelasticity and Loads, SecondEdition is an updated new edition offering comprehensivecoverage of the main principles of aircraft aeroelasticity andloads. For ease of reference, the book is divided into three partsand begins by reviewing the underlying disciplines of vibrations,aerodynamics, loads and control, and then goes on to describesimplified models to illustrate aeroelastic behaviour and aircraftresponse and loads for the flexible aircraft before introducingsome more advanced methodologies. Finally, it explains howindustrial certification requirements for aeroelasticity and loadsmay be met and relates these to the earlier theoretical approachesused. Key features of this new edition include: Uses a unified simple aeroelastic model throughout thebook Major revisions to chapters on aeroelasticity Updates and reorganisation of chapters involving FiniteElements Some reorganisation of loads material Updates on certification requirements Accompanied by a website containing a solutions manual, andMATLAB® and SIMULINK® programs that relate to the modelsused For instructors who recommend this textbook, a series oflecture slides are also available Introduction to Aircraft Aeroelasticity and Loads, SecondEdition is a must-have reference for researchers andpractitioners working in the aeroelasticity and loads fields, andis also an excellent textbook for senior undergraduate and graduatestudents in aerospace engineering.
Author : Harold A. Hamer
Release : 1961
Genre :
Kind : eBook
Book Rating : /5 ( reviews)
Book Synopsis Application of Monte Carlo Technique for Determining Maneuvering Loads from Statistical Information on Airplane Motions by : Harold A. Hamer
Download or read book Application of Monte Carlo Technique for Determining Maneuvering Loads from Statistical Information on Airplane Motions written by Harold A. Hamer. This book was released on 1961. Available in PDF, EPUB and Kindle. Book excerpt: A statistical analysis of horizontal-tail loads was made from measurements obtained on a fighter airplane during operational training. The flights covered altitudes up to about 50,000 feet and Mach numbers up to 1.22. The analysis was performed to determine the feasibility of calculating horizontal-tail load from data on the flight conditions and airplane motions. Loads were calculated by two methods, a direct approach and a Monte carlo technique, and were compared with the measured loads for each type of mission performed during the flight investigation. (Author).
Author : Ted L. Lomax
Release : 1996
Genre : Airframes
Kind : eBook
Book Rating : 185/5 ( reviews)
Book Synopsis Structural Loads Analysis by : Ted L. Lomax
Download or read book Structural Loads Analysis written by Ted L. Lomax. This book was released on 1996. Available in PDF, EPUB and Kindle. Book excerpt:
Author : Jan Robert Wright
Release : 2008-02-08
Genre : Technology & Engineering
Kind : eBook
Book Rating : 400/5 ( reviews)
Book Synopsis Introduction to Aircraft Aeroelasticity and Loads by : Jan Robert Wright
Download or read book Introduction to Aircraft Aeroelasticity and Loads written by Jan Robert Wright. This book was released on 2008-02-08. Available in PDF, EPUB and Kindle. Book excerpt: Aircraft performance is influenced significantly both by aeroelastic phenomena, arising from the interaction of elastic, inertial and aerodynamic forces, and by load variations resulting from flight and ground manoeuvres and gust / turbulence encounters. There is a strong link between aeroelasticity and loads, and these topics have become increasingly integrated in recent years. Introduction to Aircraft Aeroelasticity and Loads introduces the reader to the main principles involved in a wide range of aeroelasticity and loads topics. Divided into three sections, the book begins by reviewing the underlying disciplines of vibrations, aerodynamics, loads and control. It goes on to describe simplified models to illustrate aeroelastic behaviour and aircraft response before introducing more advanced methodologies. Finally, it explains how industrial certification requirements for aeroelasticity and loads may be met and relates these to the earlier theoretical approaches used. Presents fundamentals of structural dynamics, aerodynamics, static and dynamic aeroelasticity, response and load calculations and testing techniques. Covers performance issues related to aeroelasticity such as flutter, control effectiveness, divergence and redistribution of lift. Includes up-to-date experimental methods and analysis. Accompanied by a website with MatLAB and SIMULINK programs that relate to the models used. Introduction to Aircraft Aeroelasticity and Loads enables the reader to understand the aeroelastic and loads principles and procedures employed in a modern aircraft design office. It will appeal to final year undergraduate and masters students as well as engineers who are new to the aerospace industry.
