Development of advanced methods of structural and trajectory analysis for transport aircraftfinal report : October 1, 1995-February 28, 1998 : NASA Ames Research Center grant NCC2-5167
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National Aeronautics and Space Administration, National Technical Information Service, distributor , [Washington, DC, Springfield, Va
Supersonic transports., Optimization., Aircraft performance., Perturbation., Trajectory analysis., Cost effectiveness., Fuel consump
|Statement||Mark D. Ardema, principal investigator.|
|Series||[NASA contractor report] -- NASA/CR-207770., NASA contractor report -- NASA CR-207770.|
|Contributions||United States. National Aeronautics and Space Administration.|
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"Development of Advanced Methods of Structural and Trajectory Analysis for Transport Aircraft," during the first year of the grant October 1, - Septem The effort was in two areas: (1) development of advanced methods of structural weight estimation, and (2) development ofadvanced methods of flight path optimization.
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Get this from a library. Development of advanced methods of structural and trajectory analysis for transport aircraft: annual report: October 1, - Septem [Mark D Ardema; United States.
National Aeronautics and Space Administration.]. Development of advanced methods of structural and trajectory analysis for transport aircraft. Technical Report CR, NASA, Mar.
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Based on the author's best-selling book Aircraft Structures for Engineering Students, this brief text introduces the reader to the basics of structural analysis as applied to aircraft structures. Coverage of elasticity, energy methods and virtual work sets the stage for discussions Book Edition: 1.
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Karnovsky and O. Lebed, Advanced Methods of Structural Analysis, DOI / 2, c Springer Science+Business Media, LLC 15 16 2 General Theory of Inﬂuence Lines only that position of the load is arbitrary, i.e., this is a static load, which may have different positions along.
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A unique feature of this book is the discussion Drag Analysis of Transport Aircraft Case.  Seshadri B. R., Krishnamurthy T. and Ross R. W., “ Characterization of Aircraft Structural Damage Using Guided Wave Based Finite Element Analysis for in-Flight Structural Health Management,” 24th AIAA/AHS Adaptive Structures Conference, AIAA Science and Technology Forum and ExpositionAIAA PaperJan.
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No assumptions are made with regard to the method of analysis. All As with the first edition, this textbook provides a clear introduction to the fundamental theory of structural analysis as applied to vehicles, aircraft 3/5(1).
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Based on the author's best-selling text Aircraft Structures for Engineering Students, this brief book covers the basics of structural analysis as applied to aircraft structures.
Coverage of elasticity, energy methods, and virtual work sets the stage for discussions Book Edition: 2. The development of an integrated tool capable of determining the resources required (fuel and operational time) for a given aircraft trajectory, as well as assessing its environmental impact, is.
The book reflects author personal experience rather than a focus on all aspects of actual aircraft structural loading, which makes the author focuses on wing, landing gear, and empennage loads and gives minor attention to the semi-monocoque fuselage loading; and fully ignores the gyroscopic loads due to yawing and pitching which imposes loads on the engine attachments and supporting structure /5(4).
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Book This book does not require a rating on the project's quality scale. high structural safety record. Aircraft experiences variable loading in services. Rarely an aircraft will fail due to static overload during its service life.
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Fundamentals of Aircraft Structural Analysis focuses on the basics behind the elements of aircraft structural analysis using an applications-oriented approach. Through the use of extensive practical problems, Howard Curtis introduces your undergraduate students to the theory required for understanding linear, static structural behavior, and the /5(11).
conceptual aircraft design methods is employed. Configuration-specific critical loads are evaluated and used for sizing the structure. A gradient-free optimization algorithm is used to optimize the fuel burn of a generic long-range wide-body transport aircraft configuration with 9 shape parameters.
First results show a File Size: 1MB. This report summarizes the efforts in two areas: (1) development of advanced methods of structural weight estimation, and (2) development of advanced methods of trajectory optimization. The authors and their colleagues developed this text over many years, teaching undergraduate and graduate courses in structural analysis courses at the Daniel Guggenheim School of Aerospace Engineering of the Georgia Institute of Technology.
The emphasis is on clarity and unity in the presentation of basic structural analysis concepts and methods.For space transport purposes, we want to know how useful a structural material is in and of itself, rather than as part of a vehicle with other propulsion.
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