Aerodynamic Studies
Author : Zbiginew Krzywoblocki
Publisher :
Page : 122 pages
File Size : 44,65 MB
Release : 1957
Category : Aerodynamics
ISBN :
Author : Zbiginew Krzywoblocki
Publisher :
Page : 122 pages
File Size : 44,65 MB
Release : 1957
Category : Aerodynamics
ISBN :
Author : Holt Ashley
Publisher : Courier Corporation
Page : 306 pages
File Size : 44,84 MB
Release : 1965-01-01
Category : 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 :
Page : 21 pages
File Size : 27,58 MB
Release : 1992
Category : Aeronautics
ISBN :
Author : Richard W. Ziemer
Publisher :
Page : 52 pages
File Size : 42,51 MB
Release : 1958
Category : 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 : Helen Louise Reed
Publisher :
Page : 12 pages
File Size : 19,92 MB
Release : 2001
Category : 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 : Michael S. Selig
Publisher : Soartech
Page : 320 pages
File Size : 18,57 MB
Release : 1995
Category : Technology & Engineering
ISBN :
Author : Dietrich Küchemann
Publisher : AIAA Education
Page : 0 pages
File Size : 46,25 MB
Release : 2012
Category : Technology & Engineering
ISBN : 9781600869228
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.
Author :
Publisher :
Page : 306 pages
File Size : 38,69 MB
Release : 1964
Category : Science
ISBN :
Author :
Publisher :
Page : 8 pages
File Size : 12,64 MB
Release : 1981
Category : Aerodynamics
ISBN :
Author : John D. Anderson, Jr
Publisher : Cambridge University Press
Page : 498 pages
File Size : 47,42 MB
Release : 1999-01-28
Category : Technology & Engineering
ISBN : 1139935992
From the Foreword: 'John Anderson's book represents a milestone in aviation literature. For the first time aviation enthusiasts - both specialists and popular readers alike - possess an authoritative history of aerodynamic theory. Not only is this study authoritative, it is also highly readable and linked to the actual (and more familiar) story of how the airplane evolved. The book touches on all the major theorists and their contributions and, most important, the historical context in which they worked to move the science of aerodynamics forward.' Von Hardesty, Smithsonian Institution From the reviews: 'Something of the unexpected quality of this book can be inferred from its full title A History of Aerodynamics and Its Impact on Flying Machines. Pilots tend to suppose that the science of aerodynamics began empirically, somewhere around the time of Lilienthal and the Wrights, and that aerodynamics and manned flight are roughly coeval. It is therefore surprising to come upon a photograph of the Wright Flyer as late as page 242 of the 478-page volume.' Peter Garrison, Flying 'This book successfully straddles the boundary that separates a text book from a history book. It is of equal interest to both the aerodynamicist and the layman. The textual balance achieved by the author has resulted in a book that is enjoyable and educational.' Earl See, American Aviation Historical Society Newsletter