Transonics

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Lessons in Transonics

Author : Glen C. Cutlip
Publisher : Xlibris Corporation
Page : 214 pages
File Size : 43,8 Mb
Release : 2020-10-11
Category : Philosophy
ISBN : 9781664135208

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Lessons in Transonics by Glen C. Cutlip Pdf

This Book as well as all other books and manuscripts, published or yet unpublished, written by the author, began after a dream experience in which I was encouraged to write.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.

Fluid Dynamics for the Study of Transonic Flow

Author : Heinrich J. Ramm
Publisher : Oxford University Press
Page : 211 pages
File Size : 40,9 Mb
Release : 1990-02-01
Category : Science
ISBN : 9780195362954

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Fluid Dynamics for the Study of Transonic Flow by Heinrich J. Ramm Pdf

This 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.

Introduction to Transonic Aerodynamics

Author : Roelof Vos,Saeed Farokhi
Publisher : Springer
Page : 555 pages
File Size : 50,8 Mb
Release : 2015-03-04
Category : Technology & Engineering
ISBN : 9789401797474

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Introduction to Transonic Aerodynamics by Roelof Vos,Saeed Farokhi Pdf

Written 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.

Transonic Investigation of the Static Longitudinal Aerodynamic Characteristics of Low-aspect-ratio Wing-body Configurations at Angles of Attack from 00 to 900

Author : Charles D. Trescot,Lawrence E. Putman,Cuyler W. Brooks
Publisher : Unknown
Page : 48 pages
File Size : 51,9 Mb
Release : 1963
Category : Aerodynamics
ISBN : UIUC:30112106598011

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Transonic Investigation of the Static Longitudinal Aerodynamic Characteristics of Low-aspect-ratio Wing-body Configurations at Angles of Attack from 00 to 900 by Charles D. Trescot,Lawrence E. Putman,Cuyler W. Brooks Pdf

The Transonic Consciousness

Author : Glen C. Cutlip
Publisher : Xlibris Corporation
Page : 206 pages
File Size : 46,5 Mb
Release : 2001-10-15
Category : Body, Mind & Spirit
ISBN : 9781462801558

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The Transonic Consciousness by Glen C. Cutlip Pdf

The Transonic Sacrifice

Author : Glen C. Cutlip
Publisher : Xlibris Corporation
Page : 193 pages
File Size : 52,9 Mb
Release : 2020-03-20
Category : Philosophy
ISBN : 9781796094534

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The Transonic Sacrifice by Glen C. Cutlip Pdf

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Transonic Aerodynamic Characteristics of a Variable-sweep Airplane Configuration Having a 12-percent-thick Wing and an Inboard Pivot Location

Author : Ralph P. Bielat,P. Kenneth Pierpont
Publisher : Unknown
Page : 84 pages
File Size : 44,5 Mb
Release : 1960
Category : Aerodynamics
ISBN : UIUC:30112104458143

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Transonic Aerodynamic Characteristics of a Variable-sweep Airplane Configuration Having a 12-percent-thick Wing and an Inboard Pivot Location by Ralph P. Bielat,P. Kenneth Pierpont Pdf

A Method of Calibrating Airspeed Installations on Airplanes at Transonic and Supersonic Speeds by the Use of Accelerometer and Attitude-angle Measurements

Author : Carl Kaplan,Frank M. Hamaker,George B. Brajnikoff,Harry L. Runyan,John A. Zalovcik,John C. Martin,John M. Riebe,M. M. Frocht,United States. National Advisory Committee for Aeronautics
Publisher : Unknown
Page : 252 pages
File Size : 44,9 Mb
Release : 1953
Category : Aerodynamics, Hypersonic
ISBN : OSU:32435025004763

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A Method of Calibrating Airspeed Installations on Airplanes at Transonic and Supersonic Speeds by the Use of Accelerometer and Attitude-angle Measurements by Carl Kaplan,Frank M. Hamaker,George B. Brajnikoff,Harry L. Runyan,John A. Zalovcik,John C. Martin,John M. Riebe,M. M. Frocht,United States. National Advisory Committee for Aeronautics Pdf

Transonic Aerodynamics

Author : J.D. Cole,L.P. Cook
Publisher : Elsevier
Page : 482 pages
File Size : 55,6 Mb
Release : 2012-12-02
Category : Transportation
ISBN : 9780444599063

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Transonic Aerodynamics by J.D. Cole,L.P. Cook Pdf

This self-contained book begins with fundamental principles and proceeds to the latest developments in the field. Using a systematic mathematical approach, it covers linearized and transonic theories, simple flows, general theories of lift and drag, subsonic flows, sonic flows, shock waves, airfoils and three-dimensional wings. Also discussed are far fields and the transonic law of stabilization.Significant mathematical areas which enter the discussion are: Partial Differential Equations of Mixed Type, Weak Solutions (Shock Waves), Hodograph Transformations, Similarity Solutions and New Numerical Methods for Equations of Mixed Type.

On Transonic Flow Past a Wave-shaped Wall

Author : Carl Kaplan
Publisher : Unknown
Page : 52 pages
File Size : 54,9 Mb
Release : 1952
Category : Aerodynamics, Transonic
ISBN : UOM:39015086495879

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On Transonic Flow Past a Wave-shaped Wall by Carl Kaplan Pdf

The simplified nonlinear differential equation for transonic flow past a wavy wall is solved by the method of integration in series. A general procedure for the solution of the resulting recurrence formulas is shown and illustrated by a number of examples. A numerical test of convergence is applied to a key power series in k, the transonic similartiy parameter, and leads to the conclusion that smooth symmetrical potential flow past the wavy wall is no longer possible when the critical value of the stream Mach number is exceeded.