Автор: Scott W. Palmer Название: Dictatorship of the Air ISBN: 0521859573 ISBN-13(EAN): 9780521859578 Издательство: Cambridge Academ Рейтинг: Цена: 36220.00 T Наличие на складе: Есть Описание: Focusing on one of the last untold chapters in the history of human flight, Dictatorship of the Air is the first book to explain the true story behind twentieth-century Russia`s quest for aviation prominence. Based on nearly a decade of scholarly research, but written with general readers in mind, this is the only account to answer the question `What is `Russian` about Russian aviation?`
Автор: Gregory Название: Introduction to Flight Testing of Light Aircraft a nd UAVs ISBN: 111894982X ISBN-13(EAN): 9781118949825 Издательство: Wiley Рейтинг: Цена: 88650.00 T Наличие на складе: Есть у поставщика Поставка под заказ. Описание:
Provides an introduction to the basic flight testing methods employed on general aviation aircraft and unmanned aerial vehicles
Introduction to Flight Testing of Light Aircraft and UAVs provides a concise introduction to the basic flight testing methods employed on general aviation aircraft and unmanned aerial vehicles for courses in aeronautical engineering. There is particular emphasis on the use of modern on-board instruments and inexpensive, off-the-shelf portable devices that make flight testing accessible to nearly any student.
This text presents a clear articulation of standard methods for measuring aircraft performance characteristics. Topics covered include aircraft and instruments, digital data acquisition techniques, flight test planning, the standard atmosphere, uncertainty analysis, level flight performance, airspeed calibration, stall, climb and glide, take-off and landing, level turn, and static and dynamic longitudinal stability.
Unique to this book is a detailed discussion of digital data acquisition (DAQ) techniques, which are an integral part of modern flight test programs. This treatment includes discussion of the analog-to-digital conversion, sample rate, aliasing, and filtering. These critical details provide the flight test engineer with the insight needed to understand the capabilities and limitations of digital DAQ.
Key features:
Provides an introduction to the basic flight testing methods and instrumentation employed on general aviation aircraft and unmanned aerial vehicles.
Includes examples of flight testing on general aviation aircraft such as Cirrus, Piper, and Cessna aircraft, along with unmanned aircraft vehicles.
Suitable for courses on Aircraft Flight Test Engineering.
Introduction to Flight Testing of Light Aircraft and UAVs provides resources and guidance for practitioners in the rapidly-developing field of UAV performance flight test and the general aviation flight test community.
Автор: Norbert Kroll; Rolf Radespiel; Jan Willem van der Название: Computational Flight Testing ISBN: 3662511061 ISBN-13(EAN): 9783662511060 Издательство: Springer Рейтинг: Цена: 130590.00 T Наличие на складе: Есть у поставщика Поставка под заказ. Описание: This book reports on the ComFliTe research initiative to enhance numerical simulation of flight physics. Covers improved physical modeling, more efficient handling of aircraft control surfaces and better simulation of flight maneuvers like gust encounter.
Автор: Norbert Kroll; Rolf Radespiel; Jan Willem van der Название: Computational Flight Testing ISBN: 3642388760 ISBN-13(EAN): 9783642388767 Издательство: Springer Рейтинг: Цена: 156720.00 T Наличие на складе: Есть у поставщика Поставка под заказ. Описание: This book reports on the ComFliTe research initiative to enhance numerical simulation of flight physics. Covers improved physical modeling, more efficient handling of aircraft control surfaces and better simulation of flight maneuvers like gust encounter.
Автор: Mackowski Maura Phillips Название: Testing the Limits: Aviation Medicine and the Origins of Manned Space Flight ISBN: 1623498171 ISBN-13(EAN): 9781623498177 Издательство: Mare Nostrum (Eurospan) Рейтинг: Цена: 23410.00 T Наличие на складе: Есть у поставщика Поставка под заказ. Описание: In 1958 the United States launched its first satellite and created the National Aeronautics and Space Administration (NASA) to oversee its new space program. By 1961 NASA was confident enough to put a human being into space. But how had it acquired enough medical knowledge to ensure an astronaut’s safety in just three years? It hadn’t. The credit goes instead to decades of military medical research. Witnessing the first German missile attack on London in 1944, U.S. Army flight surgeon Harry Armstrong had been immediately concerned that aeronautical engineers would transform the A-4 (V-2) into a vehicle for transporting soldiers. He vowed, as founder (in 1934) of the military’s only aviation human-factors research lab, to make such trips survivable. Efforts at Wright Field and the army’s School of Aviation Medicine, which Armstrong had also turned into a world-class research institution, were the real reason for the successful start to America’s manned space program. In Testing the Limits , Maura Phillips Mackowski describes the crucial foundational contributions of military flight surgeons who routinely risked their lives in test aircraft, research balloons, pressure chambers, rocket-propelled sleds, or parachute harnesses. Drawing on rare primary sources and interviews, she also reveals the little-known but vital contributions of German emigré scientists whose expertise in areas unknown to Americans created a hybrid specialty: space medicine. She reveals new details on human aeromedical experimentation at Dachau, Washington’s decision to limit astronaut status to males, and the choice to freeze the air force out of the research specialty it had created and brought to fruition.
Accelerated testing (most types of laboratory testing, proving ground testing, intensive field/flight testing, any experimental research) is increasingly a key component for predicting of product's/process performance.
Trends in Development Accelerated Testing for Automotive and Aerospace Engineering provides a completely updated analysis of the current status of accelerated testing, including the basic general directions of testing (methods and equipment) development, how one needs to study real world conditions for their accurate simulation and successful accelerated testing, describes in details the role of accurate simulation in the development of automotive and aerospace engineering, shows that failures are most often found in the interconnections, step-by-step instructions and examples. This is the only book presently available that considers in detail both the positive and negative trends in testing development for prediction quality, reliability, safety, durability, maintainability, supportability, profit, and decreasing life-cycle cost, recalls, complaints and other performance components of the product. The author presents new ideas and offers a unique strategic approach to obtaining solutions which were not possible using earlier. His methodology has been widely implemented, continue to be adopted throughout the world, and leads to advance society through product improvement that can reduce loss of life, injuries, financial losses, and product recalls.
It also covers new ideas in development positive and cost- effective trends in testing development, especially accelerated reliability and durability testing (ART/ADT), which includes integration accurate simulation of field/flight influences, safety, human factors, and leads to successful prediction of product performance during pre-design, design, manufacturing, and usage for the product's service life.
Engineers, researchers, teachers and postgraduate/advanced students who are involved in automotive and aerospace engineering will find this a useful reference on how to apply the accelerated testing method to solve practical problems in these areas.
Автор: Lee Kyong Hwa Название: Amazing Paper Airplanes: The Craft and Science of Flight ISBN: 0826356648 ISBN-13(EAN): 9780826356642 Издательство: Mare Nostrum (Eurospan) Рейтинг: Цена: 16680.00 T Наличие на складе: Нет в наличии. Описание: In this book Kyong Hwa Lee combines the art of origami and the science of flight to create unique paper airplane designs for aviation enthusiasts of all ages. Featuring thirty-two designs, Amazing Paper Airplanes showcases models resembling real-world aircraft, including the F-22 fighter jet, a P-51 World War II plane, the Convair F-102 Delta Dagger—the first supersonic delta-wing interceptor airplane of the US Air Force—and more. For these models, Lee provides information along with an image of the real plane to encourage interest in aerospace technology. Every design has been flight-tested and presents complete step-by-step folding instructions. In addition to showing basic and advanced folding techniques and providing templates for each plane, the author explains the theory behind flight and offers tips to fine-tune paper airplanes for optimal flying.
Автор: Konstantinos Kanistras; Kimon P. Valavanis; Matthe Название: Foundations of Circulation Control Based Small-Scale Unmanned Aircraft ISBN: 3319884964 ISBN-13(EAN): 9783319884967 Издательство: Springer Рейтинг: Цена: 93160.00 T Наличие на складе: Поставка под заказ. Описание: This book focuses on using and implementing Circulation Control (CC) - an active flow control method used to produce increased lift over the traditionally used systems, like flaps, slats, etc. - to design a new type of fixed-wing unmanned aircraft that are endowed with improved aerodynamic efficiency, enhanced endurance, increased useful payload (fuel capacity, battery cells, on-board sensors) during cruise flight, delayed stall, and reduced runway during takeoff and landing. It presents the foundations of a step-by-step comprehensive methodology from design to implementation and experimental testing of Coand? based Circulation Control Wings (CCWs) and CC system, both integral components of the new type of aircraft, called Unmanned Circulation Control Air Vehicle. The methodology is composed of seven coupled phases: theoretical and mathematical analysis, design, simulation, 3-D printing/prototyping, wind tunnel testing, wing implementation and integration, and flight testing. The theoretical analysis focuses on understanding the physics of the flow and on defining the design parameters of the geometry restrictions of the wing and the plenum. The design phase centers on: designs of Coand? surfaces based on wing geometry specifications; designing and modifying airfoils from well-known ones (NACA series, Clark-Y, etc.); plenum designs for flow uniformity; dual radius flap designs to delay flow separation and reduce cruise drag. The simulation phase focuses on Computational Fluid Dynamics (CFD) analysis and simulations, and on calculating lift and drag coefficients of the designed CCWs in a simulation environment. 3-D printing and prototyping focuses on the actual construction of the CCWs. Wind tunnel testing centers on experimental studies in a laboratory environment. One step before flight testing is implementation of the qualified CCW and integration on the UAV platform, along with the CC system. Flight testing is the final phase, where design validation is performed. This book is the first of its kind, and it is suitable for students and researchers interested in the design and development of CCWs for small-scale aircraft. Background knowledge on fundamental Aerodynamics is required.
Автор: Walker, John R. Название: British Nuclear Weapons and the Test Ban 1954–1973 ISBN: 113838397X ISBN-13(EAN): 9781138383975 Издательство: Taylor&Francis Рейтинг: Цена: 50010.00 T Наличие на складе: Есть у поставщика Поставка под заказ. Описание: Focusing on a key twenty year period, this study explores Britain's role in efforts to bring about a nuclear test ban treaty between 1954 and 1973. Taking a broadly chronological approach, it examines the nature of defence planning, Anglo-American relationships, the efficacy of British diplomacy and UK contributions to arms control and disarmament. The appraisal of the relationship between the requirements and developments of the UK nuclear weapons programme against the countervailing international and domestic pressures for a test ban treaty will be of interest to anyone studying post-war British defence and foreign policy, history of science, arms control, disarmament and non-proliferation and international relations, or who is looking for background information on current events involving nuclear proliferation and disarmament.
Автор: Walber Chad, Walter Patrick, Seidlitz Steve Название: Sensors and Instrumentation, Aircraft/Aerospace, Energy Harvesting & Dynamic Environments Testing, Volume 7: Proceedings of the 38th Imac, a Conferenc ISBN: 3030477126 ISBN-13(EAN): 9783030477127 Издательство: Springer Цена: 186330.00 T Наличие на складе: Есть у поставщика Поставка под заказ. Описание: Sensors and Instrumentation, Aircraft/Aerospace and Energy Harvesting, Volume 7: Proceedings of the 38th IMAC, A Conference and Exposition on Structural Dynamics, 2020, the seventh volume of eight from the Conference brings together contributions to this important area of research and engineering.
Автор: Walber Chad, Walter Patrick, Seidlitz Steve Название: Sensors and Instrumentation, Aircraft/Aerospace, Energy Harvesting & Dynamic Environments Testing, Volume 7: Proceedings of the 37th Imac, a Conferenc ISBN: 3030126781 ISBN-13(EAN): 9783030126780 Издательство: Springer Рейтинг: Цена: 186330.00 T Наличие на складе: Есть у поставщика Поставка под заказ. Описание: Chapter1: Historical Review of "Building Block Approach" in Validation for Human Space Flight.- Chapter2: Analytically Investigating Impedence-Matching Test Fixtures.- Chapter3: Harmonic Forcing of Damped Non-homogeneous Elastic Rods.- Chapter4: Effects of Multi-Axial versus Single-Axial Excitation of Jointed Systems.- Chapter5: Quantifying the Effect of Component Inertial Properties on System Level Dynamics.- Chapter6: A Method for Determining Impact Force for Single and Tri Axis Resonant Plate Shock Simulations.- Chapter7: Non-stationarity and non-Gaussianity in Vibration Fatigue.- Chapter8: Use of Topology Optimization to Design Shock and Vibration Test Fixtures.- Chapter9: Electromechanical Impedance Method for Applications in Boundary Condition Replication.- Chapter10: Latest Design Trends in Modal Accelerometers for Aircraft Ground Vibration Testing.- Chapter11: Test-Based Uncertainty Quantification and Propagation using Hurty/Craig-Bampton Substructure Representations.- Chapter12: Accumulated Lifetimes in Single-Axis Vibration Testing.- Chapter13: Instrumentation and Data Acquisition Mistakes in a Structural Dynamic Facility and How to Learn from Them.- Chapter14: Adaptive Multi-modal Tuned Mass Dampers Based on Shape Memory Alloys: Design and Validation.- Chapter15: Application of Transfer Path Analysis Techniques to the Boundary Condition Challenge Problem.- Chapter16: Testing Summary for the Box Assembly with Removable Component Structure.- Chapter17: Comparison of Multi-Axis Testing of the BARC Structure with Varying Boundary Conditions.- Chapter18: Strategies for Shaker Placement for Impedance-Matched Multi-Axis Testing.- Chapter19: Comparison of Vibration Comfort Criteria by Controlled Field Tests on An Existing Long-span Floor.- Chapter20: Flight Environments Demonstrator: Part III - Sensitivity of Expansion to Model Accuracy.- Chapter21: Force Estimation Methods and Numerical Corrections for IMMAT Test Design.- Chapter22: Input Signal Synthesis for Open-loop Multiple-input/Multiple-output Testing.- Chapter23: Combining Test and Simulation to Tackle the Challenges Derived from Boundary Conditions Mismatches in Environmental Testing.- Chapter24: Defining Component Environments and Margin through Zemblanic Consideration of Function Spaces.- Chapter25: European Service Module - Structural Test Article (E-STA) Building Block Test Approach and Model Correlation Observations.- Chapter26: Control of Plate Vibrations with Artificial Neural Networks and Piezoelectricity.- Chapter27: Comparing Fixed-Base and Shaker Table Model Correlation Methods using Jim Beam.- Chapter28: Vibration Reduction for Camera Systems Onboard Small Unmanned Aircraft.- Chapter29: Flight Environments Demonstrator: Part I - Experiment Design & Test Planning.- Chapter30: Replicating Responses: Environmental Testing of Unknown Boundary Conditions.- Chapter31: An Approach to Component Testing: An Analytical Study.- Chapter32: Issues in Laboratory Simulation of Field Vibration Data: Experimental Results of a Typical Structure.- Chapter33: Clamping Force Effects on the Performance of Mechanically Attached Piezoelectric Transducers for Impedance-Based NDE.- Chapter34: Data Based Modeling of Aero Engine Vibration Responses.- Chapter35: Experimental Mode Verification (EMV) using Left-Hand Eigenvectors.- Chapter36: Understanding Multi-Axis Resonant Plate Shock Response.- Chapter37: Generating Anechoic Traveling Wave in Beams with Various Boundary Conditions.- Chapter38: Flexible Data Acquisition System Design and Architecture for a Multi-force Testing Facility.- Chapter39: Monitoring of Environmental and Sound-induced Vibrations on Artistic Stained Glasses.- Chapter40: Sensitivity Study of BARC Assembly.
Название: Adhesive bonding of aircraft composite structures ISBN: 3319928090 ISBN-13(EAN): 9783319928098 Издательство: Springer Рейтинг: Цена: 46570.00 T Наличие на складе: Есть у поставщика Поставка под заказ. Описание: The book reports the optimal use of composite materials to allow weight savings, reduction in fuel consumptions, savings during production and higher cost efficiency for ground operations.
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