Aerodynamic Studies
Author | : Zbiginew Krzywoblocki |
Publisher | : |
Total Pages | : 122 |
Release | : 1957 |
Genre | : Aerodynamics |
ISBN | : |
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Author | : Zbiginew Krzywoblocki |
Publisher | : |
Total Pages | : 122 |
Release | : 1957 |
Genre | : Aerodynamics |
ISBN | : |
Author | : Holt Ashley |
Publisher | : Courier Corporation |
Total Pages | : 306 |
Release | : 1965-01-01 |
Genre | : Technology & Engineering |
ISBN | : 0486648990 |
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.
Author | : National Research Council (U.S.). Committee on Aeronautical Technologies |
Publisher | : |
Total Pages | : 21 |
Release | : 1992 |
Genre | : Aeronautics |
ISBN | : |
Author | : Michael S. Selig |
Publisher | : Soartech |
Total Pages | : 320 |
Release | : 1995 |
Genre | : Technology & Engineering |
ISBN | : |
Author | : Richard W. Ziemer |
Publisher | : |
Total Pages | : 52 |
Release | : 1958 |
Genre | : Electromagnetic waves |
ISBN | : |
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).
Author | : Bruno Chanetz |
Publisher | : Springer Nature |
Total Pages | : 329 |
Release | : 2020-01-03 |
Genre | : Science |
ISBN | : 3030355624 |
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.
Author | : Helen Louise Reed |
Publisher | : |
Total Pages | : 12 |
Release | : 2001 |
Genre | : Computational fluid dynamics |
ISBN | : |
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.
Author | : Langley Research Center |
Publisher | : |
Total Pages | : 380 |
Release | : 1971 |
Genre | : Aeronautics |
ISBN | : |
Author | : United States. National Aeronautics and Space Administration |
Publisher | : |
Total Pages | : 792 |
Release | : |
Genre | : |
ISBN | : |