Author: Martin J. BrennerPublisher:
ISBN:
Category : Aeroelasticity
Languages : en
Pages : 34
Book Description
Overview of Recent Flight Flutter Testing Research at NASA Dryden
Author: Martin J. BrennerPublisher:
ISBN:
Category : Aeroelasticity
Languages : en
Pages : 34
Book Description
Flutter Substantiation of Transport Category Airplanes
Author: United States. Federal Aviation AdministrationPublisher:
ISBN:
Category : Aircraft carriers
Languages : en
Pages : 20
Book Description
Introduction to Aircraft Aeroelasticity and Loads
Author: Jan Robert WrightPublisher: John Wiley & Sons
ISBN: 0470858400
Category : Technology & Engineering
Languages : en
Pages : 527
Book Description
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.
Flutter Studies of Simplified Component Models of a Variable-sweep-wing Airplane at Mach Numbers Up to 3.0
Author: Maynard C. SandfordPublisher:
ISBN:
Category : Airplanes
Languages : en
Pages : 50
Book Description
Transonic Flutter Investigation of Models of the X-15 Airplane Horizontal Tail
Author: Lou S. YoungPublisher:
ISBN:
Category : Aerodynamic measurements
Languages : en
Pages : 40
Book Description
Interstage Adapter Panel Flutter on Atlas- Centaur AC-2, AC-3, and AC-4 Vehicles
Author: Tilak R. LallPublisher:
ISBN:
Category : Flutter (Aerodynamics)
Languages : en
Pages : 20
Book Description
Introduction to Structural Dynamics and Aeroelasticity
Author: Dewey H. HodgesPublisher: Cambridge University Press
ISBN: 9781139433914
Category : Technology & Engineering
Languages : en
Pages : 186
Book Description
Aeroelastic and structural dynamic phenomena play an important role in many facets of engineering. In particular, an understanding of these disciplines is essential to the design of aircraft and space vehicles. This text provides an introduction to structural dynamics and aeroelasticity, with an emphasis on conventional aircraft. The primary areas considered are structural dynamics, static aeroelasticity, and dynamic aeroelasticity. The structural dynamics material emphasizes vibration, the modal representation, and dynamic response. Aeroelastic phenomena discussed include divergence, aileron reversal, airload redistribution, unsteady aerodynamics, flutter, and elastic tailoring. Both exact and approximate solution methodologies are stressed. More than one hundred illustrations and tables help clarify the text, while upwards of fifty problems enhance student learning.
Flutter Design of Stiffened-skin Panels for Hypersonic Aircraft
Author: Herman L. BohonPublisher:
ISBN:
Category : Aerodynamics, Hypersonic
Languages : en
Pages : 36
Book Description
Design factors for flutter control of stiffened exterior skin panels for hypersonic aircraft.
Scientific and Technical Aerospace Reports
Author: Whirl Flutter of Turboprop Aircraft Structures
Author: Jiří ČečrdlePublisher: Elsevier
ISBN: 0323955568
Category : Technology & Engineering
Languages : en
Pages : 378
Book Description
Whirl Flutter of Turboprop Aircraft Structures, Second Edition explores the whirl flutter phenomenon, including theoretical, practical, analytical and experimental aspects of the matter. Sections provide a general overview regarding aeroelasticity, discussions on the physical principle and the occurrence of whirl flutter in aerospace practice, and experimental research conducted, especially from the 60s. Other chapters delve into analytical methods such as basic and advanced linear models, non-linear and CFD based methods, certification issues including regulation requirements, a description of possible certification approaches, and several examples of aircraft certification from aerospace. Finally, a database of relevant books, reports and papers is provided. This updated and expanded second edition covers new chapters including both analytical and experimental aspects of the subject matter. - Provides complex information on turboprop aircraft whirl flutter phenomenon - Presents both theoretical and practical (certification related) issues - Includes experimental research as well as analytical models (basic and advanced) of matter - Includes both early-performed works and recent developments - Contains a listing of relevant books and reports