ISAC: A Tool for Aeroservoelastic Modeling and Analysis

ISAC: A Tool for Aeroservoelastic Modeling and Analysis PDF Author:
Publisher:
ISBN:
Category :
Languages : en
Pages : 16

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ISAC: A Tool for Aeroservoelastic Modeling and Analysis

ISAC: A Tool for Aeroservoelastic Modeling and Analysis PDF Author:
Publisher:
ISBN:
Category :
Languages : en
Pages : 16

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Book Description


Scientific and Technical Aerospace Reports

Scientific and Technical Aerospace Reports PDF Author:
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 568

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Computational Aerodynamic Modeling of Aerospace Vehicles

Computational Aerodynamic Modeling of Aerospace Vehicles PDF Author: Mehdi Ghoreyshi
Publisher: MDPI
ISBN: 3038976105
Category : Technology & Engineering
Languages : en
Pages : 294

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Book Description
Currently, the use of computational fluid dynamics (CFD) solutions is considered as the state-of-the-art in the modeling of unsteady nonlinear flow physics and offers an early and improved understanding of air vehicle aerodynamics and stability and control characteristics. This Special Issue covers recent computational efforts on simulation of aerospace vehicles including fighter aircraft, rotorcraft, propeller driven vehicles, unmanned vehicle, projectiles, and air drop configurations. The complex flow physics of these configurations pose significant challenges in CFD modeling. Some of these challenges include prediction of vortical flows and shock waves, rapid maneuvering aircraft with fast moving control surfaces, and interactions between propellers and wing, fluid and structure, boundary layer and shock waves. Additional topic of interest in this Special Issue is the use of CFD tools in aircraft design and flight mechanics. The problem with these applications is the computational cost involved, particularly if this is viewed as a brute-force calculation of vehicle’s aerodynamics through its flight envelope. To make progress in routinely using of CFD in aircraft design, methods based on sampling, model updating and system identification should be considered.

Aeroservoelastic Simulation of an Active Flexible Wing Wind Tunnel Model

Aeroservoelastic Simulation of an Active Flexible Wing Wind Tunnel Model PDF Author: Carey S. Buttrill
Publisher:
ISBN:
Category : Flutter (Aerodynamics)
Languages : en
Pages : 64

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Multidisciplinary Design Optimization

Multidisciplinary Design Optimization PDF Author: Natalia M. Alexandrov
Publisher: SIAM
ISBN: 9780898713596
Category : Design
Languages : en
Pages : 476

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Book Description
Multidisciplinary design optimization (MDO) has recently emerged as a field of research and practice that brings together many previously disjointed disciplines and tools of engineering and mathematics. MDO can be described as a technology, environment, or methodology for the design of complex, coupled engineering systems, such as aircraft, automobiles, and other mechanisms, the behavior of which is determined by interacting subsystems.

Monthly Catalog of United States Government Publications

Monthly Catalog of United States Government Publications PDF Author:
Publisher:
ISBN:
Category : Government publications
Languages : en
Pages :

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Structures Technology for Future Aerospace Systems

Structures Technology for Future Aerospace Systems PDF Author: Ahmed Khairy Noor
Publisher: AIAA
ISBN: 9781600864407
Category : Airframes
Languages : en
Pages : 472

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A Collection of Technical Papers

A Collection of Technical Papers PDF Author:
Publisher:
ISBN:
Category : Aerodynamics
Languages : en
Pages : 636

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Monthly Catalogue, United States Public Documents

Monthly Catalogue, United States Public Documents PDF Author:
Publisher:
ISBN:
Category : Government publications
Languages : en
Pages : 1064

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Modeling the Benchmark Active Control Technology Wind-tunnel Model for Active Control Design Applications

Modeling the Benchmark Active Control Technology Wind-tunnel Model for Active Control Design Applications PDF Author: Martin R. Waszak
Publisher:
ISBN:
Category : Aeroelasticity
Languages : en
Pages : 34

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Book Description
This report describes the formulation of a model of the dynamic behavior of the Benchmark Active Controls Technology (BACT) wind tunnel for active control design and analysis applications. The model is formed by combining the equations of motion for the BACT wind tunnel model with actuator models and a model of wind tunnel turbulence. The primary focus of this report is the development of the equations of motion from first principles by using Lagrange's equations and the principle of virtual work. A numerical form of the model is generated by making use of parameters obtained from both experiment and analysis. Comparisons between experimental and analytical data obtained from the numerical model show excellent agreement and suggest that simple coefficient-based aerodynamics are sufficient to accurately characterize the aeroelastic response of the BACT wind tunnel model. The equations of motion developed herein have been used to aid in the design and analysis of a number of flutter suppresion controllers that have been successfully implemented.