A Historical Overview of Flight Flutter Testing PDF Download
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Author: Michael W. Kehoe
Publisher:
ISBN:
Category : Flutter (Aerodynamics)
Languages : en
Pages : 24
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Book Description
Author: Michael W. Kehoe
Publisher:
ISBN:
Category : Flutter (Aerodynamics)
Languages : en
Pages : 24
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Book Description
Author:
Publisher: DIANE Publishing
ISBN: 1428995803
Category :
Languages : en
Pages : 115
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Book Description
Author: Ralph D. Kimberlin
Publisher: AIAA
ISBN: 9781600860560
Category : Airplanes
Languages : en
Pages : 464
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Book Description
Annotation The measurement of performance during an airplane's flight, testing is one of the more important tasks to be accomplished during its development as it impacts on both the airplane's safety and its marketability. This book discusses performance for both propeller-driven and jet aircraft.
Author: Martin J. Brenner
Publisher:
ISBN:
Category : Aeroelasticity
Languages : en
Pages : 34
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Book Description
Author: Air Force Missile Development Center (U.S.)
Publisher:
ISBN:
Category : Guided missiles
Languages : en
Pages : 334
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Book Description
Author:
Publisher:
ISBN:
Category :
Languages : en
Pages : 118
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Book Description
Author: Alejandro Sobron
Publisher: Linköping University Electronic Press
ISBN: 9176852202
Category :
Languages : en
Pages : 130
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Book Description
Downscaled physical models, also referred to as subscale models, have played an essential role in the investigation of the complex physics of flight until the recent disruption of numerical simulation. Despite the fact that improvements in computational methods are slowly pushing experimental techniques towards a secondary role as verification or calibration tools, real-world testing of physical prototypes still provides an unmatched confidence. Physical models are very effective at revealing issues that are sometimes not correctly identified in the virtual domain, and hence can be a valuable complement to other design tools. But traditional wind-tunnel testing cannot always meet all of the requirements of modern aeronautical research and development. It is nowadays too expensive to use these scarce facilities to explore different design iterations during the initial stages of aircraft development, or to experiment with new and immature technologies. Testing of free-flight subscale models, referred to as Subscale Flight Testing (SFT), could offer an affordable and low-risk alternative for complementing conventional techniques with both qualitative and quantitative information. The miniaturisation of mechatronic systems, the advances in rapid-prototyping techniques and power storage, as well as new manufacturing methods, currently enable the development of sophisticated test objects at scales that were impractical some decades ago. Moreover, the recent boom in the commercial drone industry has driven a quick development of specialised electronics and sensors, which offer nowadays surprising capabilities at competitive prices. These recent technological disruptions have significantly altered the cost-benefit function of SFT and it is necessary to re-evaluate its potential in the contemporary aircraft development context. This thesis aims to increase the comprehension and knowledge of the SFT method in order to define a practical framework for its use in aircraft design; focusing on low-cost, short-time solutions that don’t require more than a small organization and few resources. This objective is approached from a theoretical point of view by means of an analysis of the physical and practical limitations of the scaling laws; and from an empirical point of view by means of field experiments aimed at identifying practical needs for equipment, methods, and tools. A low-cost data acquisition system is developed and tested; a novel method for semi-automated flight testing in small airspaces is proposed; a set of tools for analysis and visualisation of flight data is presented; and it is also demonstrated that it is possible to explore and demonstrate new technology using SFT with a very limited amount of economic and human resources. All these, together with a theoretical review and contextualisation, contribute to increasing the comprehension and knowledge of the SFT method in general, and its potential applications in aircraft conceptual design in particular.
Author:
Publisher:
ISBN:
Category : Aeroelasticity
Languages : en
Pages : 460
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Book Description
These proceedings represent a collection of the latest advances in aeroelasticity and structural dynamics from the world community. Research in the areas of unsteady aerodynamics and aeroelasticity, structural modeling and optimazation, active control and adaptive structures, landing dynamics, certification and qualification, and validation testing are highlighted in the collection of papers. The wide range of results will lead to advances in the prediction and control of the structural response of aircraft and spacecraft.
Author: Vaughan Askue
Publisher: Iowa State Press
ISBN: 9780813813080
Category : Transportation
Languages : en
Pages : 177
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Book Description
Now that it's built, how well will it fly? Flight Testing Homebuilt Aircraft tells how to test such aircraft systematically and safely, with professional results. It defines flight testing as a four-phase step-by-step process of learning the limitations of an aircraft; defining and eliminating aircraft problems; and determining aircraft capability and optimum flying techniques - all with minimum risk to pilot and machine. With straightforward description and more than 80 illustrations, the book teaches builders to use this process to design thorough, safe flight tests customized to specific aircraft in specific testing environments.
Author: R. Allemang
Publisher: Springer Science & Business Media
ISBN: 1461424194
Category : Technology & Engineering
Languages : en
Pages : 652
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Book Description
Topics in Modal Analysis II, Volume 6: Proceedings of the 30th IMAC, A Conference and Exposition on Structural Dynamics, 2012, is the sixth volume of six from the Conference and brings together 65 contributions to this important area of research and engineering. The collection presents early findings and case studies on fundamental and applied aspects of Structural Dynamics, including papers on: Aerospace, Acoustics, Energy Harvesting, Shock and Vibration, Finite Element, Structural Health Monitoring, Biodynamics Experimental Techniques, Damage Detection, Rotating Machinery, Sports Equipment Dynamics, Aircraft/Aerospace.
