Application of approximate unsteady aerodynamics for flutter analysis

Application of approximate unsteady aerodynamics for flutter analysis PDF Author: Chan-gi Pak
Publisher:
ISBN:
Category :
Languages : en
Pages : 20

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Application of approximate unsteady aerodynamics for flutter analysis

Application of approximate unsteady aerodynamics for flutter analysis PDF Author: Chan-gi Pak
Publisher:
ISBN:
Category :
Languages : en
Pages : 20

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Book Description


Application of Approximate Unsteady Aerodynamics for Flutter Analysis

Application of Approximate Unsteady Aerodynamics for Flutter Analysis PDF Author: Nasa Technical Reports Server (Ntrs)
Publisher: BiblioGov
ISBN: 9781289195885
Category :
Languages : en
Pages : 28

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Book Description
A technique for approximating the modal aerodynamic influence coefficient (AIC) matrices by using basis functions has been developed. A process for using the resulting approximated modal AIC matrix in aeroelastic analysis has also been developed. The method requires the unsteady aerodynamics in frequency domain, and this methodology can be applied to the unsteady subsonic, transonic, and supersonic aerodynamics. The flutter solution can be found by the classic methods, such as rational function approximation, k, p-k, p, root locus et cetera. The unsteady aeroelastic analysis using unsteady subsonic aerodynamic approximation is demonstrated herein. The technique presented is shown to offer consistent flutter speed prediction on an aerostructures test wing (ATW) 2 and a hybrid wing body (HWB) type of vehicle configuration with negligible loss in precision. This method computes AICs that are functions of the changing parameters being studied and are generated within minutes of CPU time instead of hours. These results may have practical application in parametric flutter analyses as well as more efficient multidisciplinary design and optimization studies.

Aeroservoelastic Modeling and Applications Using Minimum-state Approximations of the Unsteady Aerodynamics

Aeroservoelastic Modeling and Applications Using Minimum-state Approximations of the Unsteady Aerodynamics PDF Author:
Publisher:
ISBN:
Category :
Languages : en
Pages : 16

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Introduction to Structural Dynamics and Aeroelasticity

Introduction to Structural Dynamics and Aeroelasticity PDF Author: Dewey H. Hodges
Publisher: Cambridge University Press
ISBN: 9781139433914
Category : Technology & Engineering
Languages : en
Pages : 186

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Book Description
Aeroelastic and structural dynamic phenomena play an important role in many facets of engineering. In particular, an understanding of these disciplines is essential to the design of aircraft and space vehicles. This text provides an introduction to structural dynamics and aeroelasticity, with an emphasis on conventional aircraft. The primary areas considered are structural dynamics, static aeroelasticity, and dynamic aeroelasticity. The structural dynamics material emphasizes vibration, the modal representation, and dynamic response. Aeroelastic phenomena discussed include divergence, aileron reversal, airload redistribution, unsteady aerodynamics, flutter, and elastic tailoring. Both exact and approximate solution methodologies are stressed. More than one hundred illustrations and tables help clarify the text, while upwards of fifty problems enhance student learning.

A Method of Predicting Quasi-steady Aerodynamics for Flutter Analysis of High Speed Vehicles Using Steady CFD Calculations

A Method of Predicting Quasi-steady Aerodynamics for Flutter Analysis of High Speed Vehicles Using Steady CFD Calculations PDF Author: Robert C. Scott
Publisher:
ISBN:
Category : Flutter (Aerodynamics)
Languages : en
Pages : 14

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Book Description
High speed linear aerodynamic theories like piston theory and Newtonian impact theory are relatively inexpensive to use for flutter analysis. These theories have limited areas of applicability depending on the configuration and the flow conditions. In addition, these theories lack the ability to capture viscous, shock, and real gas effects. CFD methods can model all of these effects accurately, but the unsteady calculations required for flutter are expensive and often impractical. This paper describes a method for using steady CFD calculations to approximate the generalized aerodynamic forces for a flutter analysis. Example two-and three-dimensional aerodynamic force calculations are provided. In addition, a flutter analysis of a NASP-type wing will be discussed.

Introduction to Nonlinear Aeroelasticity

Introduction to Nonlinear Aeroelasticity PDF Author: Grigorios Dimitriadis
Publisher: John Wiley & Sons
ISBN: 1118756460
Category : Technology & Engineering
Languages : en
Pages : 944

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Book Description
Introduction to Nonlinear Aeroelasticity Introduces the latest developments and technologies in the area of nonlinear aeroelasticity Nonlinear aeroelasticity has become an increasingly popular research area in recent years. There have been many driving forces behind this development, increasingly flexible structures, nonlinear control laws, materials with nonlinear characteristics and so on. Introduction to Nonlinear Aeroelasticity covers the theoretical basics in nonlinear aeroelasticity and applies the theory to practical problems. As nonlinear aeroelasticity is a combined topic, necessitating expertise from different areas, the book introduces methodologies from a variety of disciplines such as nonlinear dynamics, bifurcation analysis, unsteady aerodynamics, non-smooth systems and others. The emphasis throughout is on the practical application of the theories and methods, so as to enable the reader to apply their newly acquired knowledge Key features: Covers the major topics in nonlinear aeroelasticity, from the galloping of cables to supersonic panel flutter Discusses nonlinear dynamics, bifurcation analysis, numerical continuation, unsteady aerodynamics and non-smooth systems Considers the practical application of the theories and methods Covers nonlinear dynamics, bifurcation analysis and numerical methods Accompanied by a website hosting Matlab code Introduction to Nonlinear Aeroelasticity is a comprehensive reference for researchers and workers in industry and is also a useful introduction to the subject for graduate and undergraduate students across engineering disciplines.

Basis Function Approximation of Transonic Aerodynamic Influence Coefficient Matrix

Basis Function Approximation of Transonic Aerodynamic Influence Coefficient Matrix PDF Author: National Aeronautics and Space Adm Nasa
Publisher: Independently Published
ISBN: 9781794333284
Category : Science
Languages : en
Pages : 38

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Book Description
A technique for approximating the modal aerodynamic influence coefficients matrices by using basis functions has been developed and validated. An application of the resulting approximated modal aerodynamic influence coefficients matrix for a flutter analysis in transonic speed regime has been demonstrated. This methodology can be applied to the unsteady subsonic, transonic, and supersonic aerodynamics. The method requires the unsteady aerodynamics in frequency-domain. The flutter solution can be found by the classic methods, such as rational function approximation, k, p-k, p, root-locus et cetera. The unsteady aeroelastic analysis for design optimization using unsteady transonic aerodynamic approximation is being demonstrated using the ZAERO flutter solver (ZONA Technology Incorporated, Scottsdale, Arizona). The technique presented has been shown to offer consistent flutter speed prediction on an aerostructures test wing 2 configuration with negligible loss in precision in transonic speed regime. These results may have practical significance in the analysis of aircraft aeroelastic calculation and could lead to a more efficient design optimization cycle. Li, Wesley W. and Pak, Chan-gi Armstrong Flight Research Center NASA/TM-2011-216423, H-3082, DFRC-E-DAA-TN2479

Unsteady Transonic Aerodynamics in Frequency Domain for Flutter Analysis

Unsteady Transonic Aerodynamics in Frequency Domain for Flutter Analysis PDF Author: Tai-Hsing Tom Sun
Publisher:
ISBN:
Category :
Languages : en
Pages : 162

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Fundamentals of Aeroelasticity

Fundamentals of Aeroelasticity PDF Author: Massimo Gennaretti
Publisher: Springer Nature
ISBN: 3031533798
Category :
Languages : en
Pages : 302

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Book Description


Engineered Biomimicry

Engineered Biomimicry PDF Author: Akhlesh Lakhtakia
Publisher: Newnes
ISBN: 0123914329
Category : Science
Languages : en
Pages : 493

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Book Description
Engineered Biomimicry covers a broad range of research topics in the emerging discipline of biomimicry. Biologically inspired science and technology, using the principles of math and physics, has led to the development of products as ubiquitous as VelcroTM (modeled after the spiny hooks on plant seeds and fruits). Readers will learn to take ideas and concepts like this from nature, implement them in research, and understand and explain diverse phenomena and their related functions. From bioinspired computing and medical products to biomimetic applications like artificial muscles, MEMS, textiles and vision sensors, Engineered Biomimicry explores a wide range of technologies informed by living natural systems. Engineered Biomimicry helps physicists, engineers and material scientists seek solutions in nature to the most pressing technical problems of our times, while providing a solid understanding of the important role of biophysics. Some physical applications include adhesion superhydrophobicity and self-cleaning, structural coloration, photonic devices, biomaterials and composite materials, sensor systems, robotics and locomotion, and ultra-lightweight structures. - Explores biomimicry, a fast-growing, cross-disciplinary field in which researchers study biological activities in nature to make critical advancements in science and engineering - Introduces bioinspiration, biomimetics, and bioreplication, and provides biological background and practical applications for each - Cutting-edge topics include bio-inspired robotics, microflyers, surface modification and more