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Author: Samuel Merryisha, Parvathy Rajendran Publisher: Penerbit USM ISBN: 9674617744 Category : Technology & Engineering Languages : en Pages : 208
Book Description
The advancement of flight science and technology has shown much boom contribution towards the aircraft wing and its retrofitting. Looking into the aircraft wing variants,they have a huge range of configurations with their individualities by commercial and military usage. This book concentrates on aircraft wings with an elaborated wing introduction and is primarily concerned with aircraft wing performance. It complements other books in the market by concentrating only on aircraft wings and their functionalities.The main objective of this book is to reach the beginning graduate-level students by providing them with the basic concept behind the aircraft wing. The expected audience of the book would ideally be the high school and undergraduate students, who have much ingenuity towards aircraft wings and their concepts.
Author: Samuel Merryisha, Parvathy Rajendran Publisher: Penerbit USM ISBN: 9674617744 Category : Technology & Engineering Languages : en Pages : 208
Book Description
The advancement of flight science and technology has shown much boom contribution towards the aircraft wing and its retrofitting. Looking into the aircraft wing variants,they have a huge range of configurations with their individualities by commercial and military usage. This book concentrates on aircraft wings with an elaborated wing introduction and is primarily concerned with aircraft wing performance. It complements other books in the market by concentrating only on aircraft wings and their functionalities.The main objective of this book is to reach the beginning graduate-level students by providing them with the basic concept behind the aircraft wing. The expected audience of the book would ideally be the high school and undergraduate students, who have much ingenuity towards aircraft wings and their concepts.
Author: W. Z. Stepniewski Publisher: Courier Corporation ISBN: 0486318516 Category : Technology & Engineering Languages : en Pages : 640
Book Description
DIVClear, concise text covers aerodynamic phenomena of the rotor and offers guidelines for helicopter performance evaluation. Originally prepared for NASA. Prefaces. New Indexes. 10 black-and-white photos. 537 figures. /div
Author: David J. Peery Publisher: Courier Corporation ISBN: 048626730X Category : Science Languages : en Pages : 578
Book Description
This legendary, still-relevant reference text on aircraft stress analysis discusses basic structural theory and the application of the elementary principles of mechanics to the analysis of aircraft structures. 1950 edition.
Author: Sergio Ricci Publisher: Butterworth-Heinemann ISBN: 0081009690 Category : Technology & Engineering Languages : en Pages : 970
Book Description
Morphing Wings Technologies: Large Commercial Aircraft and Civil Helicopters offers a fresh look at current research on morphing aircraft, including industry design, real manufactured prototypes and certification. This is an invaluable reference for students in the aeronautics and aerospace fields who need an introduction to the morphing discipline, as well as senior professionals seeking exposure to morphing potentialities. Practical applications of morphing devices are presented—from the challenge of conceptual design incorporating both structural and aerodynamic studies, to the most promising and potentially flyable solutions aimed at improving the performance of commercial aircraft and UAVs. Morphing aircraft are multi-role aircraft that change their external shape substantially to adapt to a changing mission environment during flight. The book consists of eight sections as well as an appendix which contains both updates on main systems evolution (skin, structure, actuator, sensor, and control systems) and a survey on the most significant achievements of integrated systems for large commercial aircraft. Provides current worldwide status of morphing technologies, the industrial development expectations, and what is already available in terms of flying systems Offers new perspectives on wing structure design and a new approach to general structural design Discusses hot topics such as multifunctional materials and auxetic materials Presents practical applications of morphing devices
Author: Egbert Torenbeek Publisher: John Wiley & Sons ISBN: 1118568117 Category : Technology & Engineering Languages : en Pages : 452
Book Description
Although the overall appearance of modern airliners has not changed a lot since the introduction of jetliners in the 1950s, their safety, efficiency and environmental friendliness have improved considerably. Main contributors to this have been gas turbine engine technology, advanced materials, computational aerodynamics, advanced structural analysis and on-board systems. Since aircraft design became a highly multidisciplinary activity, the development of multidisciplinary optimization (MDO) has become a popular new discipline. Despite this, the application of MDO during the conceptual design phase is not yet widespread. Advanced Aircraft Design: Conceptual Design, Analysis and Optimization of Subsonic Civil Airplanes presents a quasi-analytical optimization approach based on a concise set of sizing equations. Objectives are aerodynamic efficiency, mission fuel, empty weight and maximum takeoff weight. Independent design variables studied include design cruise altitude, wing area and span and thrust or power loading. Principal features of integrated concepts such as the blended wing and body and highly non-planar wings are also covered. The quasi-analytical approach enables designers to compare the results of high-fidelity MDO optimization with lower-fidelity methods which need far less computational effort. Another advantage to this approach is that it can provide answers to “what if” questions rapidly and with little computational cost. Key features: Presents a new fundamental vision on conceptual airplane design optimization Provides an overview of advanced technologies for propulsion and reducing aerodynamic drag Offers insight into the derivation of design sensitivity information Emphasizes design based on first principles Considers pros and cons of innovative configurations Reconsiders optimum cruise performance at transonic Mach numbers Advanced Aircraft Design: Conceptual Design, Analysis and Optimization of Subsonic Civil Airplanes advances understanding of the initial optimization of civil airplanes and is a must-have reference for aerospace engineering students, applied researchers, aircraft design engineers and analysts.
Author: Thomas C. Corke Publisher: Pearson ISBN: Category : Juvenile Nonfiction Languages : en Pages : 416
Book Description
For senior-level Aerospace Engineering students dealing with the conceptual design of aircraft. The approach of this book is to demonstrate how theoretical aspects, drawn from topics on airplane aerodynamics, aircraft structures, stability and control, propulsion, and compressible flows, can be applied to produce a new conceptual aircraft design. The book cites theoretical expressions wherever possible, but also stresses the interplay of different aspects of the design which often require compromises.
Author: Mohammad H. Sadraey Publisher: John Wiley & Sons ISBN: 1118352807 Category : Technology & Engineering Languages : en Pages : 811
Book Description
A comprehensive approach to the air vehicle design process using the principles of systems engineering Due to the high cost and the risks associated with development, complex aircraft systems have become a prime candidate for the adoption of systems engineering methodologies. This book presents the entire process of aircraft design based on a systems engineering approach from conceptual design phase, through to preliminary design phase and to detail design phase. Presenting in one volume the methodologies behind aircraft design, this book covers the components and the issues affected by design procedures. The basic topics that are essential to the process, such as aerodynamics, flight stability and control, aero-structure, and aircraft performance are reviewed in various chapters where required. Based on these fundamentals and design requirements, the author explains the design process in a holistic manner to emphasise the integration of the individual components into the overall design. Throughout the book the various design options are considered and weighed against each other, to give readers a practical understanding of the process overall. Readers with knowledge of the fundamental concepts of aerodynamics, propulsion, aero-structure, and flight dynamics will find this book ideal to progress towards the next stage in their understanding of the topic. Furthermore, the broad variety of design techniques covered ensures that readers have the freedom and flexibility to satisfy the design requirements when approaching real-world projects. Key features: • Provides full coverage of the design aspects of an air vehicle including: aeronautical concepts, design techniques and design flowcharts • Features end of chapter problems to reinforce the learning process as well as fully solved design examples at component level • Includes fundamental explanations for aeronautical engineering students and practicing engineers • Features a solutions manual to sample questions on the book’s companion website Companion website - www.wiley.com/go/sadraey
Author: Richard L. Bielawa Publisher: Amer Inst of Aeronautics & ISBN: 9781563470318 Category : Aeroelasticity. Languages : en Pages : 562
Book Description
Drawing on his extensive experience as a practicing engineer, designer, educator, and researcher in rotorcraft, the author presents a comprehensive account of the fundamental concepts of structural dynamics and aeroelasticity for conventional rotary wing aircraft, as well as for the newly emerging tilt-rotor and tilt-wing concepts. Intended for use in graduate-level courses and by practicing engineers, the volume covers all of the important topics needed for the complete understanding of rotorcraft structural dynamics and aeroelasticity, including basic analysis tools, rotating beams, gyroscopic phenomena, drive system dynamics, fuselage vibrations, methods for controlling vibrations, dynamic test procedures, stability analysis, mechanical and aeromechanical instabilities of rotors and rotor-pylon assemblies, unsteady aerodynamics and flutter of rotors, and model testing. The text is further enhanced by the inclusion of problems in each chapter.
Author: Wei Shyy Publisher: Cambridge University Press ISBN: 1107067987 Category : Technology & Engineering Languages : en Pages : 321
Book Description
This is an ideal book for graduate students and researchers interested in the aerodynamics, structural dynamics and flight dynamics of small birds, bats and insects, as well as of micro air vehicles (MAVs), which present some of the richest problems intersecting science and engineering. The agility and spectacular flight performance of natural flyers, thanks to their flexible, deformable wing structures, as well as to outstanding wing, tail and body coordination, is particularly significant. To design and build MAVs with performance comparable to natural flyers, it is essential that natural flyers' combined flexible structural dynamics and aerodynamics are adequately understood. The primary focus of this book is to address the recent developments in flapping wing aerodynamics. This book extends the work presented in Aerodynamics of Low Reynolds Number Flyers (Shyy et al. 2008).
Author: Samuel Merryisha, Parvathy Rajendran
Author: Samuel Merryisha, Parvathy Rajendran
Author: W. Z. Stepniewski
Author: David J. Peery
Author: Sergio Ricci
Author: Egbert Torenbeek
Author: Thomas C. Corke
Author: Mohammad H. Sadraey
Author: Richard L. Bielawa
Author: Alan Pope
Author: Wei Shyy