Download or read book Some Problems in the Theory and Assessment of Turbo jet Engines written by Konstantin Vasil'evich Kholshchevnikov and published by . This book was released on 1964 with total page 133 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Download or read book Some Problems in the Theory and Assessment of Turbo jet Engines written by Konstantin Vasilʹevich Kholshchevnikov and published by . This book was released on 1964 with total page 156 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Download or read book Some Problems in the Theory and Assessment of Turbo jet Engines written by Konstantin Vasil'evitch Kholchtchevnikov and published by . This book was released on 1964 with total page 133 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Download or read book Some Problems in the Theory and Assessments of Turbo jet Engines written by K.V. KHOLSHCHEVNIK0V and published by . This book was released on 1964 with total page 133 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Download or read book Some Problems in the Theory and Assessment of Turbo jet Engines written by Konstantin Vasilʹevich Kholshchevnikov and published by . This book was released on 1964 with total page 156 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Download or read book Some Problems in the Theory and Asessment of Turbo jet Engines written by K.V. Kholshchevnikov and published by . This book was released on 1964 with total page 133 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Download or read book Some Problems of Turbojet Engine Theory and Calculation written by Konstantin Vasilʹevich Kholshchevnikov and published by . This book was released on 1961 with total page 324 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Download or read book Combustion Chambers for Jet Propulsion Engines written by V. S. Zuyev and published by Elsevier. This book was released on 2013-10-22 with total page 261 pages. Available in PDF, EPUB and Kindle. Book excerpt: Combustion Chambers for Jet Propulsion Engines focuses on the design of combustion chambers for turbo-jet and ramjet engines, including reheat systems. This compilation, which is a training manual for the combustion chamber course held in the Moscow Aeronautical Institute, provides a general presentation of the basic elements of the process of operation, characteristics, and design of combustion chambers. This manual is divided into two parts. Part One discusses the elements of chemical kinetics and the theory of combustion of a homogeneous mixture in gas streams. The second part is devoted to the thermodynamics of the combustion chamber; aerodynamic and thermal losses; construction of the combustion chamber; and description of the operating process. The problem concerning the effect of losses in combustion chambers on the characteristics of jet propulsion engines is also elaborated in this text. This publication is valuable to aeronautical and combustion engineering students.

Download or read book Principles of Spaceflight Propulsion written by E. M. Goodger and published by Elsevier. This book was released on 2013-10-22 with total page 192 pages. Available in PDF, EPUB and Kindle. Book excerpt: Division III. Propulsion Systems Including Fuels, Volume 6: Principles of Spaceflight Propulsion provides an introduction to the fundamentals of the processes of energy release and conversion. This book presents the developments of space technology by providing a general view of the propulsion methods available. Organized into seven chapters, this volume begins with an overview of the systems of propulsion in space that are based on the reaction thrust from an ejected jet. This text then explores the basic structural considerations together with a broad illustration of the associated sources of energy. Other chapters consider the decomposition energy release of endothermic compounds and review the methods of application to rocket propulsion. This book discusses as well the essential factors influencing the release of nuclear energy. The final chapter deals with the basis of most systems of spacecraft propulsion, which is the conversion of available energy to the kinetic energy of a propellant jet. This book is a valuable resource for engineers.

Download or read book Factors that Affect Operational Reliability of Turbojet Engines written by Lewis Center Staff and published by . This book was released on 1960 with total page 220 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Download or read book Equilibrium Operating Performance of Axial flow Turbojet Engines by Means of Idealized Analysis written by John C. Sanders and published by . This book was released on 1949 with total page 46 pages. Available in PDF, EPUB and Kindle. Book excerpt: This investigation was made for an engine in which the ratio of axial-inlet-air velocity to compressor-tip velocity is constant, which approximates operation of turbojet engines with axial-flow compressors.

Download or read book Analysis of Limitations Imposed on One spool Turbojet engine Designs by Compressors and Turbines at Flight Mach Numbers of 0 2 0 and 2 8 written by Richard H. Cavicchi and published by . This book was released on 1954 with total page 54 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Download or read book Heat Transfer in Structures written by H. Schuh and published by Elsevier. This book was released on 2014-05-16 with total page 359 pages. Available in PDF, EPUB and Kindle. Book excerpt: Heat Transfer in Structures discusses the heat flow problems directly related to structures. A large section of the book presents the heat conduction in solids. The fundamentals of the analytical method are covered briefly, while introduction on the use of semi-analytical methods is treated in detail. Various approximate methods and finite difference methods are fully explained. The description of structural elements is dealt with extensively. The subject of analogues for finding temperature distributions are briefly discussed, while similarity laws and model testing are covered more comprehensively. Another topic of interest is the heat flow inside the solid part of an ablating body which is covered in detail. Thermal conductance across interfaces and joints are analyzed. And a thorough discussion of the steady heat flow is provided. A section of the text covers the simple structural elements. The book will provide useful information to aeronautics, astronautics, mechanics, engineers, and students of the physical sciences.

Download or read book Journal of Scientific Industrial Research written by and published by . This book was released on 1965 with total page 1106 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Download or read book The Royal Engineers Journal written by and published by . This book was released on 1964 with total page 556 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Download or read book Subject Catalog written by Library of Congress and published by . This book was released on 1960 with total page 642 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Download or read book Scientific and Technical Aerospace Reports written by and published by . This book was released on with total page 994 pages. Available in PDF, EPUB and Kindle. Book excerpt: