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Author: Glen C. Cutlip
Publisher: Xlibris Corporation
Published: 2020-08-13
Total Pages: 337
ISBN-13: 1664123822
DOWNLOAD EBOOKTRANSONICS PRESENTS AN ENIGMA IN THE NATURE OF GOD AND YOU Why is it that one believes that things have happened in the past, and that things will happen in the future, yet is unable to reconcile these two extremes with the present concepts of things?
Author: Glen C. Cutlip
Publisher: Xlibris Corporation
Published: 2020-10-11
Total Pages: 214
ISBN-13: 1664135200
DOWNLOAD EBOOKThis Book as well as all other books and manuscripts, published or yet unpublished, written by the author, began after a dream experience in which I was encouraged to write. At that time, it didn’t seem possible that I could do such a thing. However, after other inner and outer experiences having taken place, the process of writing began. Although, at first, I wasn’t sure of what I would be writing about, for the writings were somehow inspired. One dream experience, of which one is not likely to forget, is the one where a being of an higher inner realm whispered in my ear, saying, “you are chosen.” But what for? I wasn’t sure at that time. Another similar dream was one in which I was given the WORD to bring back. Again, at that time, I wasn’t sure what that meant. However, after several manuscripts were written and reread by me, things began to fit into place. That is, the dream experiences were becoming a reality. Although the writings must speak for themselves, I feel now that I was chosen to present the WORD, the WORD of the Transonic Consciousness, which is the WORD embracing the realm of the end and the beginning of a cycle of time. The Transonic WORD, then, is the WORD that takes in the harvesting of a previous cycle of time, and the WORD for the beginning of a new cycle of time. Therefore, the WORD is the everlasting WORD, the everlasting gospel, as it were. Inasmuch as the WORD is the everlasting WORD, it is backed by an infinity of beings within the inner and outer realms of being.
Author: Defense Documentation Center (U.S.)
Publisher:
Published: 1963
Total Pages: 1032
ISBN-13:
DOWNLOAD EBOOKAuthor: B. H. Goethert
Publisher:
Published: 2007
Total Pages: 420
ISBN-13:
DOWNLOAD EBOOKNumerous aspects of transonic aerodynamics include wall interference corrections in conventional wind tunnels, subsonic flow in a variety of wind tunnels, and test results from transonic wind tunnels. 1961 edition.
Author:
Publisher:
Published: 1989
Total Pages: 964
ISBN-13:
DOWNLOAD EBOOKAuthor: Roelof Vos
Publisher: Springer
Published: 2015-03-04
Total Pages: 561
ISBN-13: 9401797471
DOWNLOAD EBOOKWritten to teach students the nature of transonic flow and its mathematical foundation, this book offers a much-needed introduction to transonic aerodynamics. The authors present a quantitative and qualitative assessment of subsonic, supersonic and transonic flow around bodies in two and three dimensions. The book reviews the governing equations and explores their applications and limitations as employed in modeling and computational fluid dynamics. Some concepts, such as shock and expansion theory, are examined from a numerical perspective. Others, including shock-boundary-layer interaction, are discussed from a qualitative point of view. The book includes 60 examples and more than 200 practice problems. The authors also offer analytical methods such as Method of Characteristics (MOC) that allow readers to practice with the subject matter. The result is a wealth of insight into transonic flow phenomena and their impact on aircraft design, including compressibility effects, shock and expansion waves, shock-boundary-layer interaction and aeroelasticity.
Author: Heinrich J. Ramm
Publisher: Oxford University Press
Published: 1990-02-01
Total Pages: 211
ISBN-13: 0195362950
DOWNLOAD EBOOKThis new book leads readers step-by-step through the complexities encountered as moving objects approach and cross the sound barrier. The problems of transonic flight were apparent with the very first experimental flights of scale-model rockets when the disastrous impact of shock waves and flow separations caused the aircraft to spin wildly out of control. Today many of these problems have been overcome, and this book offers an introduction to the transonic theory that has made possible many of these advances. The emphasis is on the most important basic approaches to the solution of transonic problems. The book also includes explanations of common pitfalls that must be avoided. An effort has been made to derive the most important equations of inviscid and viscous transonic flow in sufficient detail so that even novices may feel confident in their problem-solving ability. The use of computer approaches is reviewed, with references to the extensive literature in this area, while the critical shortcomings of an exclusive reliance on computational methods are also described. The book will be valuable to anyone who needs to acquire an understanding of transonic flow, including practicing engineers as well as students of fluid mechanics.
Author: Sandip K. Chakrabarti
Publisher: World Scientific
Published: 1990
Total Pages: 216
ISBN-13: 9789810202040
DOWNLOAD EBOOKThis book presents methods of studying transonic flows applicable to various astrophysical circumstances. This is the first book of its kind and efforts have been made to be as thorough as possible. It gives complete mathematical solutions for the study in this area including various shock transitions. For any theoretical astrophysicists this book is expected to be very useful as the formalism discussed can be applied to all the branches. Both axisymmetric and non-axisymmetric flows are studied.
Author: Marten T. Landahl
Publisher: CUP Archive
Published: 1989
Total Pages: 148
ISBN-13: 9780521356640
DOWNLOAD EBOOKFirst published in 1961 this monograph deals with the analysis of unsteady lift distributions of thin oscillating wings at transonic speeds. Such distributions are needed for the prediction of flutter, which tends to occur more frequently at speeds near that of sound than in any other speed regime. This book emphasises analytical methods that treat the linearised problem for simple wing planforms such as rectangular and delta wings. There is a thorough discussion of the limitations of the validity of linearised theory as well as the proper boundary conditions to be applied for the case of flows with shocks. Although the standard approach in engineering practice is to sense transonic flow calculations with the aid of direct numerical simulations on a high-speed computer, the treatment in this classic monograph is still of value in the physical insight it provides and in the reference 'exact' solutions it supplies for simplified cases that may serve as validation cases for complicated computer codes. This classic work will be of interest to aerodynamicists, fluid dynamicists and applied mathematicians.
Author: Glen C. Cutlip
Publisher: Xlibris Corporation
Published: 2001-10-15
Total Pages: 206
ISBN-13: 1462801552
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