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Aircraft Systems Integration of Air Launched Weapons

Aircraft Systems Integration of Air Launched Weapons Author Keith A. Rigby
ISBN-10 9781118519172
Release 2013-02-21
Pages 272
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From the earliest days of aviation where the pilot would drop simple bombs by hand, to the highly agile, stealthy aircraft of today that can deliver smart ordnance with extreme accuracy, engineers have striven to develop the capability to deliver weapons against targets reliably, safely and with precision. Aircraft Systems Integration of Air-Launched Weapons introduces the various aspects of weapons integration, primarily from the aircraft systems integration viewpoint, but also considers key parts of the weapon and the desired interactions with the aircraft required for successful target engagement. Key features: Addresses the broad range of subjects that relate directly to the systems integration of air-launched weapons with aircraft, such as the integration process, system and subsystem architectures, the essential contribution that open, international standards have on improving interoperability and reducing integration costs and timescales Describes the recent history of how industry and bodies such as NATO have driven the need for greater interoperability between weapons and aircraft and worked to reduce the cost and timescales associated with the systems integration of complex air-launched weapons with aircraft Explores future initiatives and technologies relating to the reduction of systems integration costs and timescales The systems integration of air-launched weapons with aircraft requires a multi-disciplinary set of engineering capabilities. As a typical weapons integration life-cycle spans several years, new engineers have to learn the skills required by on-the-job training and working with experienced weapons integrators. Aircraft Systems Integration of Air-Launched Weapons augments hands-on experience, thereby enabling the development of subject matter expertise more quickly and in a broader context than would be achieved by working through the life-cycle on one specific project. This book also serves as a useful revision source for experienced engineers in the field.



Performance of the Jet Transport Airplane

Performance of the Jet Transport Airplane Author Trevor M. Young
ISBN-10 9781118534762
Release 2017-10-25
Pages 688
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Performance of the Jet Transport Airplane has been writing in one form or another for most of life. You can find so many inspiration from Performance of the Jet Transport Airplane also informative, and entertaining. Click DOWNLOAD or Read Online button to get full Performance of the Jet Transport Airplane book for free.



Aerospace Propulsion

Aerospace Propulsion Author T. W. Lee
ISBN-10 9781118307984
Release 2013-12-31
Pages 316
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Aerospace Propulsion has been writing in one form or another for most of life. You can find so many inspiration from Aerospace Propulsion also informative, and entertaining. Click DOWNLOAD or Read Online button to get full Aerospace Propulsion book for free.



Advanced Aircraft Design

Advanced Aircraft Design Author Egbert Torenbeek
ISBN-10 9781118568095
Release 2013-05-28
Pages 440
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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.



Aircraft Flight Dynamics and Control

Aircraft Flight Dynamics and Control Author Wayne Durham
ISBN-10 9781118646809
Release 2013-07-18
Pages 312
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Aircraft Flight Dynamics and Control addresses airplane flight dynamics and control in a largely classical manner, but with references to modern treatment throughout. Classical feedback control methods are illustrated with relevant examples, and current trends in control are presented by introductions to dynamic inversion and control allocation. This book covers the physical and mathematical fundamentals of aircraft flight dynamics as well as more advanced theory enabling a better insight into nonlinear dynamics. This leads to a useful introduction to automatic flight control and stability augmentation systems with discussion of the theory behind their design, and the limitations of the systems. The author provides a rigorous development of theory and derivations and illustrates the equations of motion in both scalar and matrix notation. Key features: Classical development and modern treatment of flight dynamics and control Detailed and rigorous exposition and examples, with illustrations Presentation of important trends in modern flight control systems Accessible introduction to control allocation based on the author's seminal work in the field Development of sensitivity analysis to determine the influential states in an airplane's response modes End of chapter problems with solutions available on an accompanying website Written by an author with experience as an engineering test pilot as well as a university professor, Aircraft Flight Dynamics and Control provides the reader with a systematic development of the insights and tools necessary for further work in related fields of flight dynamics and control. It is an ideal course textbook and is also a valuable reference for many of the necessary basic formulations of the math and science underlying flight dynamics and control.



Design and Analysis of Composite Structures

Design and Analysis of Composite Structures Author Christos Kassapoglou
ISBN-10 9781118536940
Release 2013-04-23
Pages 416
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New edition updated with additional exercises and two new chapters. Design and Analysis of Composite Structures: With Applications to Aerospace Structures, 2nd Edition builds on the first edition and includes two new chapters on composite fittings and the design of a composite panel, as well additional exercises. The book enables graduate students and engineers to generate meaningful and robust designs of complex composite structures. A compilation of analysis and design methods for structural components made of advanced composites, it begins with simple parts such as skins and stiffeners and progresses through to applications such as entire components of fuselages and wings. It provides a link between theory and day-to-day design practice, using theory to derive solutions that are applicable to specific structures and structural details used in industry. Starting with the basic mathematical derivation followed by simplifications used in real-world design,Design and Analysis of Composite Structures: With Applications to Aerospace Structures, 2nd Edition presents the level of accuracy and range of applicability of each method along with design guidelines derived from experience combined with analysis. The author solves in detail examples taken from actual applications to show how the concepts can be applied, solving the same design problem with different methods based on different drivers (e.g. cost or weight) to show how the final configuration changes as the requirements and approach change. Each chapter is followed by exercises that represent specific design problems often encountered in the aerospace industry but which are also applicable in the in the automotive, marine, and construction industries. Updated to include additional exercises, that represent real design problems encountered in the aerospace industry, but which are also applicable in the in the automotive, marine, and construction industries. Includes two new chapters. One on composite fittings and another on application and the design of a composite panel. Provides a toolkit of analysis and design methods that enable engineers and graduate students to generate meaningful and robust designs of complex composite structures. Provides solutions that can be used in optimization schemes without having to run finite element models at each iteration; thus speeding up the design process and allowing the examination of many more alternatives than traditional approaches. Supported by a complete set of lecture slides and solutions to the exercises hosted on a companion website for instructors. An invaluable resource for Engineers and graduate students in aerospace engineering as well as Graduate students and engineers in mechanical, civil and marine engineering.



Introduction to Aircraft Aeroelasticity and Loads

Introduction to Aircraft Aeroelasticity and Loads Author Jan R. Wright
ISBN-10 9781118700433
Release 2014-12-16
Pages 576
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Introduction to Aircraft Aeroelasticity and Loads, Second Edition is an updated new edition offering comprehensive coverage of the main principles of aircraft aeroelasticity and loads. For ease of reference, the book is divided into three parts and begins by reviewing the underlying disciplines of vibrations, aerodynamics, loads and control, and then goes on to describe simplified models to illustrate aeroelastic behaviour and aircraft response and loads for the flexible aircraft before introducing some 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. Key features of this new edition include: Uses a unified simple aeroelastic model throughout the book Major revisions to chapters on aeroelasticity Updates and reorganisation of chapters involving Finite Elements Some reorganisation of loads material Updates on certification requirements Accompanied by a website containing a solutions manual, and MATLAB® and SIMULINK® programs that relate to the models used For instructors who recommend this textbook, a series of lecture slides are also available Introduction to Aircraft Aeroelasticity and Loads, Second Edition is a must-have reference for researchers and practitioners working in the aeroelasticity and loads fields, and is also an excellent textbook for senior undergraduate and graduate students in aerospace engineering.



Theoretical and Computational Aerodynamics

Theoretical and Computational Aerodynamics Author Tapan K. Sengupta
ISBN-10 9781118787571
Release 2014-10-20
Pages 516
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Aerodynamics has seen many developments due to the growth of scientific computing, which has caused the design cycle time of aerospace vehicles to be heavily reduced. Today computational aerodynamics appears in the preliminary step of a new design, relegating costly, time-consuming wind tunnel testing to the final stages of design. Theoretical and Computational Aerodynamics is aimed to be a comprehensive textbook, covering classical aerodynamic theories and recent applications made possible by computational aerodynamics. It starts with a discussion on lift and drag from an overall dynamical approach, and after stating the governing Navier-Stokes equation, covers potential flows and panel method. Low aspect ratio and delta wings (including vortex breakdown) are also discussed in detail, and after introducing boundary layer theory, computational aerodynamics is covered for DNS and LES. Other topics covered are on flow transition to analyse NLF airfoils, bypass transition, streamwise and cross-flow instability over swept wings, viscous transonic flow over airfoils, low Reynolds number aerodynamics, high lift devices and flow control. Key features: Blends classical theories of incompressible aerodynamics to panel methods Covers lifting surface theories and low aspect ratio wing and wing-body aerodynamics Presents computational aerodynamics from first principles for incompressible and compressible flows Covers unsteady and low Reynolds number aerodynamics Includes an up-to-date account of DNS of airfoil aerodynamics including flow transition for NLF airfoils Contains chapter problems and illustrative examples Accompanied by a website hosting problems and a solution manual Theoretical and Computational Aerodynamics is an ideal textbook for undergraduate and graduate students, and is also aimed to be a useful resource book on aerodynamics for researchers and practitioners in the research labs and the industry.



Introduction to Unmanned Aircraft Systems

Introduction to Unmanned Aircraft Systems Author Douglas M. Marshall
ISBN-10 9781439835210
Release 2016-04-19
Pages 233
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Introduction to Unmanned Aircraft Systems is the editors’ response to their unsuccessful search for suitable university-level textbooks on this subject. A collection of contributions from top experts, this book applies the depth of their expertise to identify and survey the fundamentals of unmanned aircraft system (UAS) operations. Written from a nonengineering civilian operational perspective, the book starts by detailing the history of UASs and then explores current technology and what is expected for the future. Covering all facets of UAS elements and operation—including an examination of safety procedures and human factors—this material gives readers a truly complete and practical understanding of what it takes to safely operate UASs for a variety of missions in the National Airspace System. Topics covered include: The U.S. aviation regulatory system Certificate of authorization process UAS for geospatial data Automation and autonomy in UAS Sensors and payloads With helpful end-of-chapter discussion questions, this resource is designed to give beginning university students and other new entrants to the field a comprehensive, easy-to-understand first overview of the field. The book’s broad scope also makes it useful as a foundation for professionals embarking on further study.



Introduction to UAV Systems

Introduction to UAV Systems Author Paul Fahlstrom
ISBN-10 9781118396810
Release 2012-07-11
Pages 312
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Unmanned aerial vehicles (UAVs) have been widely adopted in the military world over the last decade and the success of these military applications is increasingly driving efforts to establish unmanned aircraft in non-military roles. Introduction to UAV Systems, 4th edition provides a comprehensive introduction to all of the elements of a complete Unmanned Aircraft System (UAS). It addresses the air vehicle, mission planning and control, several types of mission payloads, data links and how they interact with mission performance, and launch and recovery concepts. This book provides enough information to encourage a student to learn more; to provide a specialist with a basic appreciation of the technical issues that drive other parts of the system and interact with their specialty; or to help a program manager understand system-level tradeoffs and know what questions to ask. Key features: Comprehensive overview of all elements of a UAS and of how they interact. Introduces the underlying concepts of key subsystems. Emphasizes system-integration issues and how they relate to subsystem design choices. Practical discussion of issues informed by lessons learned in UAV programs. Introduction to UAV Systems, 4th edition is written both for newcomers to the subject and for experienced members of the UAV community who desire a comprehensive overview at the system level. As well as being a primary text for an introductory course on UAS or a supplementary text in a course that goes into more depth in one of the individual technologies involved in a UAS, this book is a useful overview for practicing engineers, researchers, managers, and consultants interested in UAV systems.



Aircraft Aerodynamic Design

Aircraft Aerodynamic Design Author András Sóbester
ISBN-10 9780470662571
Release 2014-11-03
Pages 264
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Aircraft Aerodynamic Design has been writing in one form or another for most of life. You can find so many inspiration from Aircraft Aerodynamic Design also informative, and entertaining. Click DOWNLOAD or Read Online button to get full Aircraft Aerodynamic Design book for free.



Aircraft Digital Electronic and Computer Systems

Aircraft Digital Electronic and Computer Systems Author Mike Tooley
ISBN-10 9781136430275
Release 2012-08-21
Pages 208
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Butterworth-Heinemann’s Aircraft Engineering Principles and Practice Series provides students, apprentices and practicing aerospace professionals with the definitive resources to advance their aircraft engineering maintenance studies and career. This book provides an introduction to the principles of aircraft digital and electronic systems. It is written for anyone pursuing a career in aircraft maintenance engineering or a related aerospace engineering discipline, and in particular will be suitable for those studying for licensed aircraft maintenance engineer status as part of an EASA or FAR-147 approved course or taking Aerospace Engineering City and Guilds modules, EDEXCEL National Units, EDEXCEL Higher National Units or a Degree in aircraft engineering.



Missile Design and Systems Engineering

Missile Design and Systems Engineering Author Eugene L. Fleeman
ISBN-10 1600869084
Release 2012
Pages 879
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Presents a comprehensive review of the missile design and systems engineering process. Suitable for aerospace engineering students and professors, this book offers them an understanding of missile design, missile technologies, launch platform integration, missile system measures of merit and the missile system development process.



Aeronautical and Astronautical Resources of the Library of Congress

Aeronautical and Astronautical Resources of the Library of Congress Author Ronald S. Wilkinson
ISBN-10 UOM:39015075632631
Release 2007
Pages 463
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Aeronautical and Astronautical Resources of the Library of Congress has been writing in one form or another for most of life. You can find so many inspiration from Aeronautical and Astronautical Resources of the Library of Congress also informative, and entertaining. Click DOWNLOAD or Read Online button to get full Aeronautical and Astronautical Resources of the Library of Congress book for free.



Fundamentals of Astrodynamics

Fundamentals of Astrodynamics Author Roger R. Bate
ISBN-10 0486600610
Release 1971
Pages 455
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Teaching text developed by U.S. Air Force Academy and designed as a first course emphasizes the universal variable formulation. Develops the basic two-body and n-body equations of motion; orbit determination; classical orbital elements, coordinate transformations; differential correction; more. Includes specialized applications to lunar and interplanetary flight, example problems, exercises. 1971 edition.



Red SAM

Red SAM Author Steven J. Zaloga
ISBN-10 9781780962061
Release 2011-12-20
Pages 48
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The Russian SA-2, nicknamed "Red SAM,†? is history's dominant antiaircraft missile. In 1960 it famously downed Gary Powers' U-2 spyplane, and two years later it was one of the missiles deployed during the Cuban Missile Crisis, which almost sparked a nuclear showdown between America and the USSR. The SA-2 was also deployed in Vietnam, North Korea, Egypt, and even the Gulf War. Using photographs, color artwork, and rare accounts from the weapon's designers, Steven J Zaloga examines the missile's development, linking this to its massive impact on Cold War air campaigns, and investigates the design changes that have helped the SA-2 stand the test of time.



Morphing Aerospace Vehicles and Structures

Morphing Aerospace Vehicles and Structures Author John Valasek
ISBN-10 9781119940302
Release 2012-02-24
Pages 312
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Morphing Aerospace Vehicles and Structures provides a highly timely presentation of the state-of-the-art, future directions and technical requirements of morphing aircraft. Divided into three sections it addresses morphing aircraft, bio-inspiration, and smart structures with specific focus on the flight control, aerodynamics, bio-mechanics, materials, and structures of these vehicles as well as power requirements and the use of advanced piezo materials and smart actuators. The tutorial approach adopted by the contributors, including underlying concepts and mathematical formulations, unifies the methodologies and tools required to provide practicing engineers and applied researchers with the insight to synthesize morphing air vehicles and morphing structures, as well as offering direction for future research.