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Author : Wahyu Hendriyono
Publisher :
ISBN 13 :
Total Pages : 166 pages
Book Rating : 4.:/5 (223 download)
Download or read book Aerodynamic Load Estimation of a Manoeuvring Aircraft written by Wahyu Hendriyono and published by . This book was released on 2000 with total page 166 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Download or read book Aerodynamic Loading on Manoeuvring Aircraft written by and published by . This book was released on 2003 with total page pages. Available in PDF, EPUB and Kindle. Book excerpt:
Author : Jan R. Wright
Publisher : John Wiley & Sons
ISBN 13 : 1118700422
Total Pages : 576 pages
Book Rating : 4.1/5 (187 download)
Download or read book Introduction to Aircraft Aeroelasticity and Loads written by Jan R. Wright and published by John Wiley & Sons. This book was released on 2014-12-16 with total page 576 pages. Available in PDF, EPUB and Kindle. Book excerpt: Introduction to Aircraft Aeroelasticity and Loads, SecondEdition is an updated new edition offering comprehensivecoverage of the main principles of aircraft aeroelasticity andloads. For ease of reference, the book is divided into three partsand begins by reviewing the underlying disciplines of vibrations,aerodynamics, loads and control, and then goes on to describesimplified models to illustrate aeroelastic behaviour and aircraftresponse and loads for the flexible aircraft before introducingsome more advanced methodologies. Finally, it explains howindustrial certification requirements for aeroelasticity and loadsmay be met and relates these to the earlier theoretical approachesused. Key features of this new edition include: Uses a unified simple aeroelastic model throughout thebook Major revisions to chapters on aeroelasticity Updates and reorganisation of chapters involving FiniteElements Some reorganisation of loads material Updates on certification requirements Accompanied by a website containing a solutions manual, andMATLAB® and SIMULINK® programs that relate to the modelsused For instructors who recommend this textbook, a series oflecture slides are also available Introduction to Aircraft Aeroelasticity and Loads, SecondEdition is a must-have reference for researchers andpractitioners working in the aeroelasticity and loads fields, andis also an excellent textbook for senior undergraduate and graduatestudents in aerospace engineering.
Author : Gabriel Isakson
Publisher :
ISBN 13 :
Total Pages : 30 pages
Book Rating : 4.3/5 (91 download)
Download or read book Effect of Structural Flexibiligy on Aircraft Loading written by Gabriel Isakson and published by . This book was released on 1951 with total page 30 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Author : Harold A. Hamer
Publisher :
ISBN 13 :
Total Pages : 50 pages
Book Rating : 4.:/5 (317 download)
Download or read book Application of Monte Carlo Technique for Determining Maneuvering Loads from Statistical Information on Airplane Motions written by Harold A. Hamer and published by . This book was released on 1961 with total page 50 pages. Available in PDF, EPUB and Kindle. Book excerpt: A statistical analysis of horizontal-tail loads was made from measurements obtained on a fighter airplane during operational training. The flights covered altitudes up to about 50,000 feet and Mach numbers up to 1.22. The analysis was performed to determine the feasibility of calculating horizontal-tail load from data on the flight conditions and airplane motions. Loads were calculated by two methods, a direct approach and a Monte carlo technique, and were compared with the measured loads for each type of mission performed during the flight investigation. (Author).
Author : J. F. McCarthy (Jr)
Publisher :
ISBN 13 :
Total Pages : 90 pages
Book Rating : 4.3/5 (91 download)
Download or read book Effect of Structural Flexibiligy on Aircraft Loading written by J. F. McCarthy (Jr) and published by . This book was released on 1953 with total page 90 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Author : A. A. Kirsch
Publisher :
ISBN 13 :
Total Pages : 108 pages
Book Rating : 4.3/5 (91 download)
Download or read book Effect of Structural Flexibiligy on Aircraft Loading written by A. A. Kirsch and published by . This book was released on 1954 with total page 108 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Author : Ted L. Lomax
Publisher : AIAA
ISBN 13 : 9781600861185
Total Pages : 306 pages
Book Rating : 4.8/5 (611 download)
Download or read book Structural Loads Analysis written by Ted L. Lomax and published by AIAA. This book was released on 1996 with total page 306 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Author : Antonio Filippone
Publisher : Cambridge University Press
ISBN 13 : 113978966X
Total Pages : 665 pages
Book Rating : 4.1/5 (397 download)
Download or read book Advanced Aircraft Flight Performance written by Antonio Filippone and published by Cambridge University Press. This book was released on 2012-12-17 with total page 665 pages. Available in PDF, EPUB and Kindle. Book excerpt: This book discusses aircraft flight performance, focusing on commercial aircraft but also considering examples of high-performance military aircraft. The framework is a multidisciplinary engineering analysis, fully supported by flight simulation, with software validation at several levels. The book covers topics such as geometrical configurations, configuration aerodynamics and determination of aerodynamic derivatives, weight engineering, propulsion systems (gas turbine engines and propellers), aircraft trim, flight envelopes, mission analysis, trajectory optimisation, aircraft noise, noise trajectories and analysis of environmental performance. A unique feature of this book is the discussion and analysis of the environmental performance of the aircraft, focusing on topics such as aircraft noise and carbon dioxide emissions.
Author : S. J. Engel
Publisher :
ISBN 13 :
Total Pages : 48 pages
Book Rating : 4.3/5 (91 download)
Download or read book Effect of Structural Flexibiligy on Aircraft Loading written by S. J. Engel and published by . This book was released on 1954 with total page 48 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Author :
Publisher :
ISBN 13 :
Total Pages : 28 pages
Book Rating : 4.:/5 (317 download)
Download or read book Recent Aerodynamic Studies Applicable to High Performance Maneuvering Aircraft written by and published by . This book was released on 1966 with total page 28 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Author : Robert Rowe Gilruth
Publisher :
ISBN 13 :
Total Pages : 12 pages
Book Rating : 4.3/5 (126 download)
Download or read book Analysis of Vertical-tail Loads in Rolling Pull-out Maneuvers written by Robert Rowe Gilruth and published by . This book was released on 1944 with total page 12 pages. Available in PDF, EPUB and Kindle. Book excerpt: Summary: An analysis is presented of the vertical-tail loads to be expected as a result of abrupt aileron action in accelerated flight, as in rolls from turns or pull-outs, for example. The formulas derived show that the vertical-tail loads obtained in rolling pull-out maneuvers are directly proportional to the load factor, wing loading, and aileron effectiveness and are inversely proportional to directional stability. Sample calculations for an assumed fighter airplane are presented and discussed. It appears that critical tail loads may occur in rolling pull-out maneuvers, particularly on airplanes with good ailerons and low directional stability.
Author : Jan Robert Wright
Publisher : John Wiley & Sons
ISBN 13 : 0470858400
Total Pages : 527 pages
Book Rating : 4.4/5 (78 download)
Download or read book Introduction to Aircraft Aeroelasticity and Loads written by Jan Robert Wright and published by John Wiley & Sons. This book was released on 2008-02-08 with total page 527 pages. Available in PDF, EPUB and Kindle. Book excerpt: 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.
Author : Ted L. Lomax
Publisher : AIAA (American Institute of Aeronautics & Astronautics)
ISBN 13 :
Total Pages : 308 pages
Book Rating : 4.3/5 (91 download)
Download or read book Structural Loads Analysis for Commercial Transport Aircraft written by Ted L. Lomax and published by AIAA (American Institute of Aeronautics & Astronautics). This book was released on 1996 with total page 308 pages. Available in PDF, EPUB and Kindle. Book excerpt: This important text covers all aspects of structural loads analysis and provides some continuity between what was done on earlier airplane designs and what the current applications of the present regulations require.
Author : Thomas R. Yechout
Publisher : AIAA
ISBN 13 : 9781600860782
Total Pages : 666 pages
Book Rating : 4.8/5 (67 download)
Download or read book Introduction to Aircraft Flight Mechanics written by Thomas R. Yechout and published by AIAA. This book was released on 2003 with total page 666 pages. Available in PDF, EPUB and Kindle. Book excerpt: Based on a 15-year successful approach to teaching aircraft flight mechanics at the US Air Force Academy, this text explains the concepts and derivations of equations for aircraft flight mechanics. It covers aircraft performance, static stability, aircraft dynamics stability and feedback control.
Author : Louis V. Schmidt
Publisher : AIAA
ISBN 13 : 9781600860775
Total Pages : 426 pages
Book Rating : 4.8/5 (67 download)
Download or read book Introduction to Aircraft Flight Dynamics written by Louis V. Schmidt and published by AIAA. This book was released on 1998 with total page 426 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Author : Cloyce E. Matheny
Publisher :
ISBN 13 :
Total Pages : 30 pages
Book Rating : 4.3/5 (126 download)
Download or read book Comparison Between Calculated and Measured Loads on Wing and Horizontal Tail in Pull-up Maneuvers written by Cloyce E. Matheny and published by . This book was released on 1945 with total page 30 pages. Available in PDF, EPUB and Kindle. Book excerpt: Summary: Comparisons have been made of measured and calculated loads on the wing and the horizontal tail in pull-up maneuvers for six airplanes ranging in weight from 4,700 to 48,000 pounds. The calculated loads were based on the control motions measured in flight. The aerodynamic characteristics of the airplanes required for the calculations were either obtained directly from wind-tunnel data or computed. Good agreement was obtained between calculated and measured loads for a specified elevator deflection when reliable wind-tunnel data were available and when the airplane maneuvers were consistent with the assumptions. The fact that only fair agreement was obtained in some of the cases was attributed either to poor quantitative knowledge of the aerodynamic parameters or to the violation of the assumptions on which the method is based.
