Sujin Bureerat (32 results)

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Condition: Brand New. New. US edition. Expediting shipping for all USA and Europe orders excluding PO Box. Excellent Customer Service.

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Condition: New. 1st edition NO-PA16APR2015-KAP.

Hardcover. Condition: Brand New. 386 pages. 6.30x1.06x9.49 inches. In Stock.

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Buch. Condition: Neu. Druck auf Anfrage Neuware - Printed after ordering - This book comprehensively covers the topic of computational aeroelasticity, which is one of the main aerospace engineering disciplines. The book highlights advanced numerical techniques for practical aircraft models rather than fundamental 2D wings. It starts with gathering numerical and mathematical background required for the subject, followed by the static and dynamic finite element analyses for aircraft structural modelling using the equations of motion for rigid-body and flexible aircraft. The book subsequently outlines subsonic aerodynamic techniques which includes a steady vortex lattice/ring method, an unsteady vortex ring method, and a doublet lattice method, with the ideas for further improvement of the methods. The following chapters deal with numerical tools for fluid-structure interaction, e.g., displacement estimation using several numerical techniques, normal-wash calculation of rigid-body and flexible aircraft, and estimation of generalized aerodynamic forces matrices. The next two chapters are concerned with static and dynamic aeroelastic analyses of fixed cantilever wings and restrained and unrestrained aircraft. Static aeroelasticity includes lift and control effectiveness (trim conditions for a fixed cantilever wing), divergence, and trim conditions for rigid-body and flexible aircraft. Dynamic aeroelasticity includes flutter modelling and solution techniques, discrete and continuous gust response, and dynamic modelling of an unrestrained flexible aircraft for aeroelastic response simulation. The final chapter demonstrates design optimization related to aeroelasticity including deterministic design with single- and multi-objective optimization and design with uncertainty. This book is suitable for senior undergraduate and graduate mechanical and aerospace engineering students as well as aerospace researchers and engineers.…

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HRD. Condition: New. New Book. Shipped from UK. Established seller since 2000.

HRD. Condition: New. New Book. Shipped from UK. Established seller since 2000.

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Condition: New. Brand New! Fast Delivery This is an International Edition and ship within 24-48 hours. Deliver by FedEx and Dhl, & Aramex, UPS, & USPS and we do accept APO and PO BOX Addresses. Order can be delivered worldwide within 6-10 days and we do have flat rate for up to 2LB. Extra shipping charges will be requested if the Book weight is more than 5 LB. This Item May be shipped from India, United states & United Kingdom. Depending on your location and availability.…

Hardcover. Condition: Brand New. 208 pages. 10.00x7.00x10.24 inches. In Stock.

Condition: New. Dieser Artikel ist ein Print on Demand Artikel und wird nach Ihrer Bestellung fuer Sie gedruckt. Autor/Autorin: Tejani GhanshyamDr. Ghanshyam Tejani is an assistant professor in MED, School of Engineering, RK University, India. His research includes truss optimization, hybrid and modified metaheuristics, artificial intelligence, machine learni.…

Hardcover. Condition: new. Hardcover. This book comprehensively covers the topic of computational aeroelasticity, which is one of the main aerospace engineering disciplines. The book highlights advanced numerical techniques for practical aircraft models rather than fundamental 2D wings. It starts with gathering numerical and mathematical background required for the subject, followed by the static and dynamic finite element analyses for aircraft structural modelling using the equations of motion for rigid-body and flexible aircraft. The book subsequently outlines subsonic aerodynamic techniques which includes a steady vortex lattice/ring method, an unsteady vortex ring method, and a doublet lattice method, with the ideas for further improvement of the methods. The following chapters deal with numerical tools for fluid-structure interaction, e.g., displacement estimation using several numerical techniques, normal-wash calculation of rigid-body and flexible aircraft, and estimation of generalized aerodynamic forces matrices. The next two chapters are concerned with static and dynamic aeroelastic analyses of fixed cantilever wings and restrained and unrestrained aircraft. Static aeroelasticity includes lift and control effectiveness (trim conditions for a fixed cantilever wing), divergence, and trim conditions for rigid-body and flexible aircraft. Dynamic aeroelasticity includes flutter modelling and solution techniques, discrete and continuous gust response, and dynamic modelling of an unrestrained flexible aircraft for aeroelastic response simulation. The final chapter demonstrates design optimization related to aeroelasticity including deterministic design with single- and multi-objective optimization and design with uncertainty. This book is suitable for senior undergraduate and graduate mechanical and aerospace engineering students as well as aerospace researchers and engineers. Dynamic aeroelasticity includes flutter modelling and solution techniques, discrete and continuous gust response, and dynamic modelling of an unrestrained flexible aircraft for aeroelastic response simulation. This item is printed on demand. Shipping may be from multiple locations in the US or from the UK, depending on stock availability.…

Buch. Condition: Neu. This item is printed on demand - it takes 3-4 days longer - Neuware -This book comprehensively covers the topic of computational aeroelasticity, which is one of the main aerospace engineering disciplines. The book highlights advanced numerical techniques for practical aircraft models rather than fundamental 2D wings. It starts with gathering numerical and mathematical background required for the subject, followed by the static and dynamic finite element analyses for aircraft structural modelling using the equations of motion for rigid-body and flexible aircraft. The book subsequently outlines subsonic aerodynamic techniques which includes a steady vortex lattice/ring method, an unsteady vortex ring method, and a doublet lattice method, with the ideas for further improvement of the methods. The following chapters deal with numerical tools for fluid-structure interaction, e.g., displacement estimation using several numerical techniques, normal-wash calculation of rigid-body and flexible aircraft, and estimation of generalized aerodynamic forces matrices. The next two chapters are concerned with static and dynamic aeroelastic analyses of fixed cantilever wings and restrained and unrestrained aircraft. Static aeroelasticity includes lift and control effectiveness (trim conditions for a fixed cantilever wing), divergence, and trim conditions for rigid-body and flexible aircraft. Dynamic aeroelasticity includes flutter modelling and solution techniques, discrete and continuous gust response, and dynamic modelling of an unrestrained flexible aircraft for aeroelastic response simulation. The final chapter demonstrates design optimization related to aeroelasticity including deterministic design with single- and multi-objective optimization and design with uncertainty. This book is suitable for senior undergraduate and graduate mechanical and aerospace engineering students as well as aerospace researchers and engineers. 373 pp. Englisch.…

Condition: New. Dieser Artikel ist ein Print on Demand Artikel und wird nach Ihrer Bestellung fuer Sie gedruckt.

Hardcover. Condition: new. Hardcover. This book comprehensively covers the topic of computational aeroelasticity, which is one of the main aerospace engineering disciplines. The book highlights advanced numerical techniques for practical aircraft models rather than fundamental 2D wings. It starts with gathering numerical and mathematical background required for the subject, followed by the static and dynamic finite element analyses for aircraft structural modelling using the equations of motion for rigid-body and flexible aircraft. The book subsequently outlines subsonic aerodynamic techniques which includes a steady vortex lattice/ring method, an unsteady vortex ring method, and a doublet lattice method, with the ideas for further improvement of the methods. The following chapters deal with numerical tools for fluid-structure interaction, e.g., displacement estimation using several numerical techniques, normal-wash calculation of rigid-body and flexible aircraft, and estimation of generalized aerodynamic forces matrices. The next two chapters are concerned with static and dynamic aeroelastic analyses of fixed cantilever wings and restrained and unrestrained aircraft. Static aeroelasticity includes lift and control effectiveness (trim conditions for a fixed cantilever wing), divergence, and trim conditions for rigid-body and flexible aircraft. Dynamic aeroelasticity includes flutter modelling and solution techniques, discrete and continuous gust response, and dynamic modelling of an unrestrained flexible aircraft for aeroelastic response simulation. The final chapter demonstrates design optimization related to aeroelasticity including deterministic design with single- and multi-objective optimization and design with uncertainty. This book is suitable for senior undergraduate and graduate mechanical and aerospace engineering students as well as aerospace researchers and engineers. Dynamic aeroelasticity includes flutter modelling and solution techniques, discrete and continuous gust response, and dynamic modelling of an unrestrained flexible aircraft for aeroelastic response simulation. This item is printed on demand. Shipping may be from our UK warehouse or from our Australian or US warehouses, depending on stock availability.…

Condition: New. Print on Demand.

Buch. Condition: Neu. This item is printed on demand - Print on Demand Titel. Neuware -This book comprehensively covers the topic of computational aeroelasticity, which is one of the main aerospace engineering disciplines. The book highlights advanced numerical techniques for practical aircraft models rather than fundamental 2D wings. It starts with gathering numerical and mathematical background required for the subject, followed by the static and dynamic finite element analyses for aircraft structural modelling using the equations of motion for rigid-body and flexible aircraft. The book subsequently outlines subsonic aerodynamic techniques which includes a steady vortex lattice/ring method, an unsteady vortex ring method, and a doublet lattice method, with the ideas for further improvement of the methods. The following chapters deal with numerical tools for fluid-structure interaction, e.g., displacement estimation using several numerical techniques, normal-wash calculation of rigid-body and flexible aircraft, and estimation of generalized aerodynamic forces matrices. The next two chapters are concerned with static and dynamic aeroelastic analyses of fixed cantilever wings and restrained and unrestrained aircraft. Static aeroelasticity includes lift and control effectiveness (trim conditions for a fixed cantilever wing), divergence, and trim conditions for rigid-body and flexible aircraft. Dynamic aeroelasticity includes flutter modelling and solution techniques, discrete and continuous gust response, and dynamic modelling of an unrestrained flexible aircraft for aeroelastic response simulation. The final chapter demonstrates design optimization related to aeroelasticity including deterministic design with single- and multi-objective optimization and design with uncertainty. This book is suitable for senior undergraduate and graduate mechanical and aerospace engineering students as well as aerospace researchers and engineers.Springer Nature Customer Service Center GmbH, Europaplatz 3,69115 Heidelberg, Germany, Heidelberg 388 pp. Englisch.…

Condition: New. PRINT ON DEMAND.

Hardcover. Condition: new. Hardcover. This book comprehensively covers the topic of computational aeroelasticity, which is one of the main aerospace engineering disciplines. The book highlights advanced numerical techniques for practical aircraft models rather than fundamental 2D wings. It starts with gathering numerical and mathematical background required for the subject, followed by the static and dynamic finite element analyses for aircraft structural modelling using the equations of motion for rigid-body and flexible aircraft. The book subsequently outlines subsonic aerodynamic techniques which includes a steady vortex lattice/ring method, an unsteady vortex ring method, and a doublet lattice method, with the ideas for further improvement of the methods. The following chapters deal with numerical tools for fluid-structure interaction, e.g., displacement estimation using several numerical techniques, normal-wash calculation of rigid-body and flexible aircraft, and estimation of generalized aerodynamic forces matrices. The next two chapters are concerned with static and dynamic aeroelastic analyses of fixed cantilever wings and restrained and unrestrained aircraft. Static aeroelasticity includes lift and control effectiveness (trim conditions for a fixed cantilever wing), divergence, and trim conditions for rigid-body and flexible aircraft. Dynamic aeroelasticity includes flutter modelling and solution techniques, discrete and continuous gust response, and dynamic modelling of an unrestrained flexible aircraft for aeroelastic response simulation. The final chapter demonstrates design optimization related to aeroelasticity including deterministic design with single- and multi-objective optimization and design with uncertainty. This book is suitable for senior undergraduate and graduate mechanical and aerospace engineering students as well as aerospace researchers and engineers. Dynamic aeroelasticity includes flutter modelling and solution techniques, discrete and continuous gust response, and dynamic modelling of an unrestrained flexible aircraft for aeroelastic response simulation. This item is printed on demand. Shipping may be from our Sydney, NSW warehouse or from our UK or US warehouse, depending on stock availability.…

Buch. Condition: Neu. This item is printed on demand - it takes 3-4 days longer - Neuware -Optimization Methods for Finite Element Analysis and Design describes recent developments in Finite Element Methods (FEM). It gives a brief introduction of the applications of AI-based nature-inspired metaheuristic algorithms and machine learning (ML) at various stages of FEM. The book covers a range of state-of-the-art application areas including medical equipment, structural analysis and machinery products.It explores the applications of optimization and ML techniques in mesh smoothing, quality improvement and Laplacian and Taubin smoothing. The book also discusses the optimization of cable nets and steel frames using nature-inspired metaheuristic methods. 192 pp. Englisch.…

Hardcover. Condition: new. Hardcover. Optimization Methods for Finite Element Analysis and Design describes recent developments in Finite Element Methods (FEM). It gives a brief introduction of the applications of AI-based nature-inspired metaheuristic algorithms and machine learning (ML) at various stages of FEM. The book covers a range of state-of-the-art application areas including medical equipment, structural analysis and machinery products.It explores the applications of optimization and ML techniques in mesh smoothing, quality improvement and Laplacian and Taubin smoothing. The book also discusses the optimization of cable nets and steel frames using nature-inspired metaheuristic methods. Optimization Methods for Finite Element Analysis and Design describes recent developments in Finite Element Methods (FEM). The book covers a range of state-of-the-art application areas including medical equipment, structural analysis, and machinery products. This item is printed on demand. Shipping may be from our UK warehouse or from our Australian or US warehouses, depending on stock availability.…