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Author : Zbiginew Krzywoblocki
Publisher : Unknown
Page : 72 pages
File Size : 47,7 Mb
Release : 1957
Category : Aerodynamics
ISBN : MSU:31293025437199
Author : Zbigniew Krzywoblocki
Publisher : Unknown
Page : 246 pages
File Size : 45,7 Mb
Release : 1960
Category : Aerodynamics
ISBN : UOM:39015095330190
Author : Helen Louise Reed,William S. Saric
Publisher : Unknown
Page : 12 pages
File Size : 48,7 Mb
Release : 2001
Category : Computational fluid dynamics
ISBN : UOM:39015104953925
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 : Anonim
Publisher : Unknown
Page : 24 pages
File Size : 40,6 Mb
Release : 1988
Category : Electronic
ISBN : NASA:31769000580723
Author : Richard W. Ziemer
Publisher : Unknown
Page : 52 pages
File Size : 40,8 Mb
Release : 1958
Category : Electromagnetic waves
ISBN : UOM:39015095145796
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 : T. Cebeci
Publisher : Springer Science & Business Media
Page : 487 pages
File Size : 46,9 Mb
Release : 2012-12-06
Category : Technology & Engineering
ISBN : 9781461249269
The Third Symposium on Numerical and Physical Aspects of Aerodynamic Flows, like its immediate predecessor, was organized with emphasis on the calculation of flows relevant to aircraft, ships, and missiles. Fifty-five papers and 20 brief communications were presented at the Symposium, which was held at the California State University at Long Beach from 21 to 24 January 1985. A panel discussion was chaired by A. M. O. Smith and includeq state ments by T. T. Huang, C. E. lobe, l. Nielsen, and C. K. Forester on priorities for future research. The first lecture in memory of Professor Keith Stewartson was delivered by J. T. Stuart and is reproduced in this volume together with a selection of the papers presented at the Symposium. In Volume II of this series, papers were selected so as to provide a clear indication of the range of procedures available to represent two-dimensional flows, their physical foundation, and their predictive ability. In this volume, the emphasis is on three-dimensional flows with a section of five papers concerned with unsteady flows and a section of seven papers on three dimensional flows: The papers deal mainly with calculation methods and encompass subsonic and transonic, attached and separated flows. The selec tion has been made so as to fulfill the same purpose for three-dimensional flows as did Volume II for two-dimensional flows.
Author : Gordon N. Patterson
Publisher : Downsview, Ont. : University of Toronto, Institute for Aerospace Studies
Page : 186 pages
File Size : 53,5 Mb
Release : 1981
Category : Aerodynamics
ISBN : 0919482066
Author : Anonim
Publisher : Unknown
Page : 306 pages
File Size : 51,7 Mb
Release : 1964
Category : Science
ISBN : UOM:39015086566265
Author : Rose G Davies
Publisher : CRC Press
Page : 191 pages
File Size : 43,7 Mb
Release : 2020-04-13
Category : Technology & Engineering
ISBN : 9780429536748
Equipping readers with the ability to analyze the aerodynamic forces on an aircraft, the book provides comprehensive knowledge of the characteristics of subsonic and supersonic airflow. This book begins with the fundamental physics principles of aerodynamics, then introduces the Continuity Equation, Energy Equations, and Bernoulli’s Equation, which form the basic aerodynamic principles for subsonic airflow. It provides a thorough understanding of the forces acting on an aircraft across a range of speeds and their effects on the aircraft's performance, including a discussion on the difference in aerofoil and aircraft shapes. Aircraft stability issues are analyzed, along with the development of a boundary layer over an aerofoil, the changes of air speed and air pressure, and boundary layer separation. Readers will gain a clear understanding of the nature of airflow over aircraft during subsonic, transonic, and supersonic flight. The book emphasizes the connection between operating actions in flight and aerodynamic requirements. The content will be of interest to senior undergraduates studying to obtain their Airline Transport Pilot License (ATPL)/Airline Transport Pilot (ATP) certificate, general aviation and air transport pilots, and aircraft maintenance engineers.
Author : Anonim
Publisher : Unknown
Page : 42 pages
File Size : 48,9 Mb
Release : 1984
Category : Electronic
ISBN : NASA:31769000562283
Author : Lewis Research Center
Publisher : Unknown
Page : 542 pages
File Size : 40,5 Mb
Release : 1965
Category : Axial flow compressors
ISBN : STANFORD:36105113764901
Author : Theodore Von Kármán
Publisher : Courier Corporation
Page : 226 pages
File Size : 49,5 Mb
Release : 2004-01-01
Category : Technology & Engineering
ISBN : 0486434850
Charming, reader-friendly chronicle by a famous pioneer in aerodynamic research traces the development of dynamic flight from the time of Newton through the 20th century. It recounts struggles of engineers and physicists with problems associated with lift, drag, stability, aeroelasticity, and the sound barrier. 72 figures. 1957 edition.
Author : Robert O. Bullock
Publisher : Unknown
Page : 552 pages
File Size : 40,9 Mb
Release : 1965
Category : Axial flow compressors
ISBN : NASA:31769000652464
Author : Peter Thiede
Publisher : Springer Science & Business Media
Page : 382 pages
File Size : 43,6 Mb
Release : 2013-06-29
Category : Technology & Engineering
ISBN : 9783540453598
------------------------------------------------------------ This volume contains the Proceedings of the CEAS/DragNet European Drag Reduction Conference held on 19-21 June 2000 in Potsdam, Germany. This conference, succeeding the European Fora on Laminar Flow Technology 1992 and 1996, was initiated by the European Drag Reduction Network (DragNet) and organised by DGLR under the auspice of CEAS. The conference addressed the recent advances in all areas of drag reduction research, development, validation and demonstration including laminar flow technology, adaptive wing concepts, turbulent and induced drag reduction, separation control and supersonic flow aspects. This volume which comprises more than 40 conference papers is of particular interest to engineers, scientists and students working in the aeronautics industry, research establishments or academia.
Author : Claus Weiland
Publisher : Springer Science & Business Media
Page : 360 pages
File Size : 42,7 Mb
Release : 2014-02-22
Category : Technology & Engineering
ISBN : 9783642541681
The capacity and quality of the atmospheric flight performance of space flight vehicles is characterized by their aerodynamic data bases. A complete aerodynamic data base would encompass the coefficients of the static longitudinal and lateral motions and the related dynamic coefficients. In this book the aerodynamics of 27 vehicles are considered. Only a few of them did really fly. Therefore the aerodynamic data bases are often not complete, in particular when the projects or programs were more or less abruptly stopped, often due to political decisions. Configurational design studies or the development of demonstrators usually happen with reduced or incomplete aerodynamic data sets. Therefore some data sets base just on the application of one of the following tools: semi-empirical design methods, wind tunnel tests, numerical simulations. In so far a high percentage of the data presented is incomplete and would have to be verified. Flight mechanics needs the aerodynamic coefficients as function of a lot of variables. The allocation of the aerodynamic coefficients for a particular flight operation at a specific trajectory point is conducted by an aerodynamic model. The establishment of such models is described in this book. This book is written for graduate and doctoral students to give them insight into the aerodynamics of the various flight configurations. Further for design and development engineers in industry and at research institutes (including universities) searching for an appropriate vehicle shape, as well as for non-specialists, who may be interested in this subject. The book will be helpful, too, in the case that system studies require in their concept phases the selection of suitable vehicle shapes.