Aerodynamic Studies

Aerodynamic Studies PDF Author: Zbiginew Krzywoblocki
Publisher:
ISBN:
Category : Aerodynamics
Languages : en
Pages : 122

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Book Description

Aerodynamic Studies

Aerodynamic Studies PDF Author: Zbiginew Krzywoblocki
Publisher:
ISBN:
Category : Aerodynamics
Languages : en
Pages : 122

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Book Description


Aerodynamics of Wings and Bodies

Aerodynamics of Wings and Bodies PDF Author: Holt Ashley
Publisher: Courier Corporation
ISBN: 0486648990
Category : Technology & Engineering
Languages : en
Pages : 306

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Book Description
This excellent, innovative reference offers a wealth of useful information and a solid background in the fundamentals of aerodynamics. Fluid mechanics, constant density inviscid flow, singular perturbation problems, viscosity, thin-wing and slender body theories, drag minimalization, and other essentials are addressed in a lively, literate manner and accompanied by diagrams.

Aeronautical Technologies for the Twenty-first Century

Aeronautical Technologies for the Twenty-first Century PDF Author: National Research Council (U.S.). Committee on Aeronautical Technologies
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 21

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Book Description


Summary of Low Speed Airfoil Data

Summary of Low Speed Airfoil Data PDF Author: Michael S. Selig
Publisher: Soartech
ISBN:
Category : Technology & Engineering
Languages : en
Pages : 320

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Book Description


Experimental and Analytical Research on the Aerodynamics of Wind Driven Turbines

Experimental and Analytical Research on the Aerodynamics of Wind Driven Turbines PDF Author: C. Rohrbach
Publisher:
ISBN:
Category : Wind power
Languages : en
Pages : 266

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Book Description


An Electromagnetic Shock Tube for Aerodynamic Research

An Electromagnetic Shock Tube for Aerodynamic Research PDF Author: Richard W. Ziemer
Publisher:
ISBN:
Category : Electromagnetic waves
Languages : en
Pages : 52

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Book Description
An electromagnetically driven shock tube was studied as a possible new tool for aerodynamic research in which velocities of up to 41,000 feet per second are obtainable in air. At these high velocities stagnation temperatures of about 35,000K are produced. The simple construction and operation of the shock tube is described and an evaluation is made of its performance. The potentialities and limitations of the apparatus are discussed with regards to research applications. The results of some magnetoaerodynamic studies are presented to show the usefulness of this type of shock tube. (Author).

Experimental Aerodynamics

Experimental Aerodynamics PDF Author: Bruno Chanetz
Publisher: Springer Nature
ISBN: 3030355624
Category : Science
Languages : en
Pages : 329

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Book Description
This book presents experimental techniques in the field of aerodynamics, a discipline that is essential in numerous areas, such as the design of aerial and ground vehicles and engines, the production of energy, and understanding the wind resistance of buildings. Aerodynamics is not only concerned with improving the performance and comfort of vehicles, but also with reducing their environmental impact. The book provides updated information on the experimental and technical methods used by aerodynamicists, engineers and researchers. It describes the various types of wind tunnels – from subsonic to hypersonic – as well as the problems posed by their design and operation. The book also focuses on metrology, which has allowed us to gain a detailed understanding of the local properties of flows, and examines current developments toward creating a methodology combining experiments and numerical simulations: the computer-assisted wind tunnel. Lastly, it offers an overview of experimental aerodynamics based on a prospective vision of the discipline, and discusses potential futures challenges. The book can be used as a textbook for graduate courses in aerodynamics, typically offered to students of aerospace and mechanical engineering programs, and as a learning tool for professionals and engineers in the fields of aerodynamics, aeronautics and astronautics automobile.

Aerodynamic Studies of Micro Air Vehicles

Aerodynamic Studies of Micro Air Vehicles PDF Author: Helen Louise Reed
Publisher:
ISBN:
Category : Computational fluid dynamics
Languages : en
Pages : 12

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Book Description
The program at Arizona State University (ASU) consisted of complementary experimental, computational, and flight-test elements that examined the aerodynamics of Micro Aerial Vehicles (MAVs). All these components supported the actual design of our MAV, called MAVRIC (Micro Aerial Vehicle Research Initiative and Competition) and which competed for two years against other university teams. MAVs are characterized by low operating chord Reynolds numbers and thus present challenges in viscous aerodynamics. Our studies focused on the effects on performance of different wing-body-juncture and wing-tip designs. MAV aerodynamics is strongly affected by the wing-tip vortices which extend over a significant amount of span. Blending the wing and fuselage and adding winglets provided a reduction in the extent of these vortices as well as a refocusing of them away from the lifting surface.

Research in Aeronautics and Space

Research in Aeronautics and Space PDF Author: Langley Research Center
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 380

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Book Description


The Aerodynamic Design of Aircraft

The Aerodynamic Design of Aircraft PDF Author: Dietrich Küchemann
Publisher: AIAA Education
ISBN: 9781600869228
Category : Technology & Engineering
Languages : en
Pages : 0

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Book Description
Dietrich Kuchemann's The Aerodynamic Design of Aircraft is as relevant and as forward looking today as it was when it was first published in 1978. It comprises the philosophy and life's work of a unique and visionary intellect. Based upon material taught in a course at Imperial College London, the insight and intuition conveyed by this text are timeless. With its republication, Kuchemann's influence will extend to the next generation of aerospace industry students and practitioners and the vehicles they will produce. Kuchemann establishes three classes of aircraft based on the character of flow involved. Each class is suitable for a distinct cruise speed regime: classical and swept aircraft for subsonic and transonic cruise, slender-wing aircraft for supersonic cruise, and wave-rider aircraft for hypersonic cruise. Unlike most engineering texts, which focus on a set of tools, Kuchemann's approach is to focus on the problem and its solution - what kind of flow is best for a given class of aircraft and how to achieve it.With this approach, Kuchemann fully embraces the true inverse nature of design; rather than answer what flow given the shape, he strives to answer what flow given the purpose and then what shape given the flow.