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Thermal Stress Determination Techniques For Supersonic Transport Aircraft Structures
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Book Synopsis Thermal Stress Determination Techniques for Supersonic Transport Aircraft Structures by : Richard H. Gallagher
Download or read book Thermal Stress Determination Techniques for Supersonic Transport Aircraft Structures written by Richard H. Gallagher and published by . This book was released on 1964 with total page 115 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Thermal Stress Determination Techniques for Supersonic Transport Aircraft Structures by : R. H. Gallagher
Download or read book Thermal Stress Determination Techniques for Supersonic Transport Aircraft Structures written by R. H. Gallagher and published by . This book was released on 1964 with total page 116 pages. Available in PDF, EPUB and Kindle. Book excerpt: This report describes computer programs developed for the analysis of heated beams, plates, and stiffened cylindrical shells. The matrix displacement approach to structural analysis, which forms the theoretical basis of these programs, is developed in detail. Derivation of new relationships employed in these programs is also detailed. The capabilities and limitations of the respective programs are outlined and illustrative applications are presented. (Author).
Book Synopsis Thermal Stress Determination Techniques for Supersonic Transport Aircraft Structures. Part Ii Design Data for Sandwich Plates and Cylinders Under Applied Loads and Thermal Gradients by : R. A. Gellatly
Download or read book Thermal Stress Determination Techniques for Supersonic Transport Aircraft Structures. Part Ii Design Data for Sandwich Plates and Cylinders Under Applied Loads and Thermal Gradients written by R. A. Gellatly and published by . This book was released on 1964 with total page 117 pages. Available in PDF, EPUB and Kindle. Book excerpt: Structural design data are presented for various applied load and thermal gradient conditions for flat rectangular sandwich panels and sandwich cylinders. The flat panel solutions pertain to instability under nonuniform stress, and also to the stresses and displacements resulting from normal pressures and temperature gradients across the panel thickness in the presence of uniform midplane compression. Sandwich cylinder design data are given for buckling under nonuniform circumferential and axial stress, respectively, and for stresses due to radial or axial temperature gradients. The range of stiffness parameters extend, at one limit, to the isotropic forms of construction. (Author).
Download or read book Technical Abstract Bulletin written by and published by . This book was released on with total page 684 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Author :United States. Federal Aviation Agency. Library Services Division Publisher : ISBN 13 : Total Pages :52 pages Book Rating :4.3/5 (243 download)
Book Synopsis Commercial Supersonic Transport Aircraft Research Program by : United States. Federal Aviation Agency. Library Services Division
Download or read book Commercial Supersonic Transport Aircraft Research Program written by United States. Federal Aviation Agency. Library Services Division and published by . This book was released on 1963 with total page 52 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis NASA Research on Materials Applicable to Supersonic Transports by : Herbert F. Hardrath
Download or read book NASA Research on Materials Applicable to Supersonic Transports written by Herbert F. Hardrath and published by . This book was released on 1964 with total page 24 pages. Available in PDF, EPUB and Kindle. Book excerpt: National Aeronautics and Space Administration has conducted tests to determine the mechanical properties of materials suitable for use in a supersonics transport over the temperature range of interest and after prolonged exposure to temperature. On the basis of studies on fatigue behavior, rate of fatigue crack propagation, residual static strength, and resistance to deterioration of properties due to prolonged exposure to temperature, no serious materials problems are anticipated. However, stress corrosion is found to be a potentially serious problem in titanium alloys in a hot salt environment and in stainless steels in an ambient environment. The-Ti-8A1-lMo-lV alloy is found to be generally superior to other contending materials in all respects studied except for salt stress corrosion in which respect it was poorer than all others. Further research is recommended on stress corrosion; on the combined effects of fatigue, thermal exposure, and creep; and on the development of structural configurations and fabrication procedures suitable for the supersonic transport.
Book Synopsis On the Calculation of Temperature Distribution and Thermal Stresses in Parts of Aircraft Structures at Supersonic Speeds by : H. Schuh
Download or read book On the Calculation of Temperature Distribution and Thermal Stresses in Parts of Aircraft Structures at Supersonic Speeds written by H. Schuh and published by . This book was released on 1955 with total page pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Thermal Stress Analysis for Aircraft Structures by : Bruno A. Boley
Download or read book Thermal Stress Analysis for Aircraft Structures written by Bruno A. Boley and published by . This book was released on 1957 with total page 44 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis A Method for Determining the Effect of Radiation Upon the Transient Temperature Distribution and Thermal Stresses Within an Idealized Aircraft Structure Flying at Supersonic Speed by : Hugh B. Phelps
Download or read book A Method for Determining the Effect of Radiation Upon the Transient Temperature Distribution and Thermal Stresses Within an Idealized Aircraft Structure Flying at Supersonic Speed written by Hugh B. Phelps and published by . This book was released on 1956 with total page 136 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Download or read book MAGIC written by Robert H. Mallett and published by . This book was released on 1969 with total page 234 pages. Available in PDF, EPUB and Kindle. Book excerpt: An automated general purpose system for analysis is presented. This system, identified by the aconym 'MAGIC' for 'Matrix Analysis via Generative and Interpretive Computations, ' provides a flexible framework for implementation of the finite element analysis technology. Powerful capabilities for displacement, stress and stability analyses are included in the subject MAGIC System for structural analysis. The matrix displacement method of analysis based upon finite element idealization is employed throughout. Six versatile finite elements are incorporated in the finite element library. These are: frame, shear panel, triangular cross-section ring, toroidal thin shell ring, quadrilateral thin shell and triangular thin shell elements. These finite element representations include matrices for stiffness, incremental stiffness, perstrain load, thermal load, distributed mechanical load and stress.
Download or read book Proceedings written by and published by . This book was released on 1968 with total page 1482 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Scientific and Technical Aerospace Reports by :
Download or read book Scientific and Technical Aerospace Reports written by and published by . This book was released on 1993 with total page 556 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Combustion in Advanced Gas Turbine Systems by : I. E. Smith
Download or read book Combustion in Advanced Gas Turbine Systems written by I. E. Smith and published by Elsevier. This book was released on 2014-05-17 with total page 415 pages. Available in PDF, EPUB and Kindle. Book excerpt: Cranfield International Symposium Series, Volume 10: Combustion in Advanced Gas Turbine Systems covers the proceedings of an International Propulsion Symposium, held at the College of Aeronautics in Cranfield in April 1967. The book focuses on the processes, methodologies, reactions, and transformations involved in chemical combustion. The selection first takes a look at the design considerations in advanced gas turbine combustion chambers, combustion in industrial gas turbines, and combustion development on the Rolls-Royce Spey engine. Discussions focus on mechanical condition, carbon-formation and exhaust smoke, system requirements, fuel oil ash deposition and corrosion, combustion-system design, performance requirements, types of primary zone, fuel injection, and combustion chamber types. The text then examines subsonic flow flameholder studies using a low pressure simulation technique; stabilization of hydrogen diffusion flames by flame-holders in supersonic flow at low stagnation temperatures; and augmentation systems for turbofan engines. The book takes a look at a consideration of the possible use of refractory ceramic materials for advanced combustion chamber design; cooling of flame tubes by steam injection; and combustion problems in the massive steam injection gas turbine. The selection is a valuable source of information for researchers interested in the process of combustion in advanced gas turbine systems.
Book Synopsis Thermal Stress Analyses by : David John Johns
Download or read book Thermal Stress Analyses written by David John Johns and published by Pergamon. This book was released on 1965 with total page 244 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Scientific and Technical Aerospace Reports by :
Download or read book Scientific and Technical Aerospace Reports written by and published by . This book was released on 1963 with total page 1064 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Correlation of Predicted and Measured Thermal Stresses on a Truss-type Aircraft Structure by :
Download or read book Correlation of Predicted and Measured Thermal Stresses on a Truss-type Aircraft Structure written by and published by . This book was released on 1978 with total page 62 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Author :United States. National Aeronautics and Space Administration. Office of Reliability and Quality Assurance Publisher : ISBN 13 : Total Pages :602 pages Book Rating :4.F/5 ( download)
Book Synopsis Reliability Abstracts and Technical Reviews by : United States. National Aeronautics and Space Administration. Office of Reliability and Quality Assurance
Download or read book Reliability Abstracts and Technical Reviews written by United States. National Aeronautics and Space Administration. Office of Reliability and Quality Assurance and published by . This book was released on 1968 with total page 602 pages. Available in PDF, EPUB and Kindle. Book excerpt:
