Abas ramiar (47 risultati)

PAP. Condizione: New. New Book. Shipped from UK. Established seller since 2000.

PAP. Condizione: New. New Book. Shipped from UK. Established seller since 2000.

Condizione: New.

Condizione: New. In English.

Condizione: New.

Condizione: New.

Paperback. Condizione: Brand New. 128 pages. 8.66x5.91x0.29 inches. In Stock.

Taschenbuch. Condizione: Neu. Computational Aerodynamics: FSI in Plasma Actuated Oscillating Airfoil | Application to macro and micro aerial vehicles | Abas Ramiar (u. a.) | Taschenbuch | 128 S. | Englisch | 2018 | LAP LAMBERT Academic Publishing | EAN 9786138389651 | Verantwortliche Person für die EU: BoD - Books on Demand, In de Tarpen 42, 22848 Norderstedt, info[at]bod[dot]de | Anbieter: preigu.…

PAP. Condizione: New. New Book. Shipped from UK. Established seller since 2000.

PAP. Condizione: New. New Book. Shipped from UK. Established seller since 2000.

Condizione: New.

Condizione: New.

Condizione: New.

Condizione: New.

PAP. Condizione: New. New Book. Shipped from UK. Established seller since 2000.

Condizione: New.

Condizione: New.

Condizione: New.

Condizione: New.

PAP. Condizione: New. New Book. Shipped from UK. Established seller since 2000.

PAP. Condizione: New. New Book. Shipped from UK. Established seller since 2000.

PAP. Condizione: New. New Book. Shipped from UK. Established seller since 2000.

Taschenbuch. Condizione: Neu. This item is printed on demand - it takes 3-4 days longer - Neuware -Today, aviation and aerospace science and industry is proposed as one of the indices of the scientific and technical level of countries, and also plays an important role in the safety of a country. Thus, efforts to promote industrial capabilities in this context is highly recommended by various countries. One of the important things that must be considered in designing aerial structures, in particular the aircraft wings, is interaction between the air and the elastic aircraft wing that is known as the aeroelastic phenomenon. In this book, a numerical study of two dimensional laminar incompressible flow around the oscillating NACA0012 airfoil is proceeded by using OpenFOAM. Oscillatory motion types including pitching, plunging and flapping is considered. Boundary layer control is an useful technique that can improve the aerodynamic performance of the airfoil and it can cause a delay in the stall, for higher angles of attack. Thus, for flow control on airfoil, Dielectric Barrier Discharge plasma actuator as used in two positions on the airfoil and the results obtained from imposing it for each three types of oscillating motion are compared. 128 pp. Englisch. …

Condizione: New. Print on Demand.

Taschenbuch. Condizione: Neu. nach der Bestellung gedruckt Neuware - Printed after ordering - Today, aviation and aerospace science and industry is proposed as one of the indices of the scientific and technical level of countries, and also plays an important role in the safety of a country. Thus, efforts to promote industrial capabilities in this context is highly recommended by various countries. One of the important things that must be considered in designing aerial structures, in particular the aircraft wings, is interaction between the air and the elastic aircraft wing that is known as the aeroelastic phenomenon. In this book, a numerical study of two dimensional laminar incompressible flow around the oscillating NACA0012 airfoil is proceeded by using OpenFOAM. Oscillatory motion types including pitching, plunging and flapping is considered. Boundary layer control is an useful technique that can improve the aerodynamic performance of the airfoil and it can cause a delay in the stall, for higher angles of attack. Thus, for flow control on airfoil, Dielectric Barrier Discharge plasma actuator as used in two positions on the airfoil and the results obtained from imposing it for each three types of oscillating motion are compared. …

Condizione: New. Dieser Artikel ist ein Print on Demand Artikel und wird nach Ihrer Bestellung fuer Sie gedruckt. Autor/Autorin: Ramiar AbasAbas Ramiar is an Associate Professor in Babol Noshirvani University of Technology, as well as distinguished young researcher of Mechanical Department at the university (in 2017). His research area focuses on microfluidics.…

Condizione: New. PRINT ON DEMAND.

Taschenbuch. Condizione: Neu. nach der Bestellung gedruckt Neuware - Printed after ordering - Precise manipulation of microparticles and cells is crucial for advancements in diverse fields, from disease diagnostics to advanced materials engineering. Microfluidic devices offer a promising platform for such manipulation due to their low cost, high sensitivity, and minimal sample requirements. This book introduces a novel microfluidic device that leverages dielectrophoresis (DEP) - a label-free and highly efficient technique - for continuous separation of three distinct particle populations. Unlike existing DEP-based separators, this device utilizes a uniquely configured bi-gap electrode pair, enabling enhanced separation efficiency and purity. The book details the design, fabrication, and performance evaluation of this innovative device.…

Taschenbuch. Condizione: Neu. This item is printed on demand - Print on Demand Titel. Neuware -Today, aviation and aerospace science and industry is proposed as one of the indices of the scientific and technical level of countries, and also plays an important role in the safety of a country. Thus, efforts to promote industrial capabilities in this context is highly recommended by various countries. One of the important things that must be considered in designing aerial structures, in particular the aircraft wings, is interaction between the air and the elastic aircraft wing that is known as the aeroelastic phenomenon. In this book, a numerical study of two dimensional laminar incompressible flow around the oscillating NACA0012 airfoil is proceeded by using OpenFOAM. Oscillatory motion types including pitching, plunging and flapping is considered. Boundary layer control is an useful technique that can improve the aerodynamic performance of the airfoil and it can cause a delay in the stall, for higher angles of attack. Thus, for flow control on airfoil, Dielectric Barrier Discharge plasma actuator as used in two positions on the airfoil and the results obtained from imposing it for each three types of oscillating motion are compared.VDM Verlag, Dudweiler Landstraße 99, 66123 Saarbrücken 128 pp. Englisch. …

Taschenbuch. Condizione: Neu. nach der Bestellung gedruckt Neuware - Printed after ordering - La manipulación precisa de micropartículas y células es crucial para avanzar en diversos campos, desde el diagnóstico de enfermedades hasta la ingeniería de materiales avanzados. Los dispositivos microfluídicos ofrecen una plataforma prometedora para dicha manipulación debido a su bajo coste, alta sensibilidad y mínimos requisitos de muestra. En este libro se presenta un novedoso dispositivo microfluídico que aprovecha la dielectroforesis (DEP) -una técnica altamente eficaz y libre de etiquetas- para la separación continua de tres poblaciones distintas de partículas. A diferencia de los separadores basados en DEP existentes, este dispositivo utiliza un par de electrodos bi-gap de configuración única, lo que permite mejorar la eficiencia y la pureza de la separación. El libro detalla el diseño, la fabricación y la evaluación del rendimiento de este innovador dispositivo.…