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Author : Frederick V. Pohle
Publisher :
ISBN 13 :
Total Pages : pages
Book Rating : 4.:/5 (841 download)
Download or read book The Effects of Elevated Temperatures on Aircraft Structures written by Frederick V. Pohle and published by . This book was released on 1959 with total page pages. Available in PDF, EPUB and Kindle. Book excerpt:
Author : Nicholas John Hoff
Publisher :
ISBN 13 :
Total Pages : 398 pages
Book Rating : 4.3/5 (91 download)
Download or read book High Temperature Effects in Aircraft Structures written by Nicholas John Hoff and published by . This book was released on 1958 with total page 398 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Author : Nicholas J (Nicholas John) 19 Hoff
Publisher : Hassell Street Press
ISBN 13 : 9781014339270
Total Pages : 394 pages
Book Rating : 4.3/5 (392 download)
Download or read book High Temperature Effects in Aircraft Structures written by Nicholas J (Nicholas John) 19 Hoff and published by Hassell Street Press. This book was released on 2021-09-09 with total page 394 pages. Available in PDF, EPUB and Kindle. Book excerpt: This work has been selected by scholars as being culturally important and is part of the knowledge base of civilization as we know it. This work is in the public domain in the United States of America, and possibly other nations. Within the United States, you may freely copy and distribute this work, as no entity (individual or corporate) has a copyright on the body of the work. Scholars believe, and we concur, that this work is important enough to be preserved, reproduced, and made generally available to the public. To ensure a quality reading experience, this work has been proofread and republished using a format that seamlessly blends the original graphical elements with text in an easy-to-read typeface. We appreciate your support of the preservation process, and thank you for being an important part of keeping this knowledge alive and relevant.
Author : John E. Duberg
Publisher :
ISBN 13 :
Total Pages : pages
Book Rating : 4.:/5 (11 download)
Download or read book Aircraft Structures Research at Elevated Temperatures by John E.Duberg written by John E. Duberg and published by . This book was released on 1991 with total page pages. Available in PDF, EPUB and Kindle. Book excerpt:
Author : John Edward Duberg
Publisher :
ISBN 13 :
Total Pages : 20 pages
Book Rating : 4.:/5 (375 download)
Download or read book Aircraft Structures Research at Elevated Temperatures written by John Edward Duberg and published by . This book was released on 1955 with total page 20 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Author : Carlo Ferrari
Publisher : Elsevier
ISBN 13 : 1483155021
Total Pages : 472 pages
Book Rating : 4.4/5 (831 download)
Download or read book High Temperatures in Aeronautics written by Carlo Ferrari and published by Elsevier. This book was released on 2013-10-22 with total page 472 pages. Available in PDF, EPUB and Kindle. Book excerpt: High Temperatures in Aeronautics is a compilation of the proceedings of the Symposium on High Temperatures in Aeronautics held in Turin, Italy, on September 10-12, 1962. The symposium provided a forum to discuss the applications of high temperatures in aeronautics and covers topics ranging from supersonic combustion to non-equilibrium flow through a nozzle, along with similarity parameters in radiation gas-dynamics and photoionization upstream of a strong shock wave. This volume is comprised of 17 chapters and begins with an overview of the effects and consequences of high temperature in aeronautics, followed by an analysis of experimental results for the dissociation of diatomic gases. A theoretical and experimental investigation of mixing and supersonic combustion is then presented, focusing on inviscid flow fields with a finite rate chemistry for a hydrogen-air reaction. Turbulent mixing for flows with large density gradients having no chemical reaction is also considered, and the results of experiments in supersonic combustion are discussed. Subsequent chapters deal with silicon nitride, its properties, and its potential use at elevated temperatures; materials problems at high temperature; and the corrosion of refractory alloys by oil ash containing vanadium. This monograph will be of interest to students, engineers, and experimental workers in the fields of astronautics and aeronautical engineering.
Author : C. D. Brownfield
Publisher :
ISBN 13 :
Total Pages : 118 pages
Book Rating : 4.3/5 (91 download)
Download or read book Effects of Temperature-time-stress Histories on the Mechanical Properties of Aircraft Structural Metallic Materials written by C. D. Brownfield and published by . This book was released on 1960 with total page 118 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Author : Richard R. Heldenfels
Publisher :
ISBN 13 :
Total Pages : 22 pages
Book Rating : 4.:/5 (722 download)
Download or read book A Summary of NACA Research on the Strength and Creep of Aircraft Structures at Elevated Temperatures written by Richard R. Heldenfels and published by . This book was released on 1956 with total page 22 pages. Available in PDF, EPUB and Kindle. Book excerpt: This paper summarizes some NACA research on the strength and creep of aircraft structural elements and components at elevated temperatures. Experimental data for aluminum-alloy columns, plates, stiffened panels, and multiweb box beams are presented for temperature up to 600 degrees F and compared with results predicted from materials data. Methods are described for predicting maximum strength from materials stress-strain curves and creep lifetime from isochronous stress-strain curves. Some observations on the probable effect of creep on the design of aircraft structures are also included to illustrate the influence of design criteria on the weight of aircraft structures at elevated temperatures.
Author : Stanford University. Department of Aeronautical Engineering
Publisher :
ISBN 13 :
Total Pages : 102 pages
Book Rating : 4.F/5 ( download)
Download or read book Effects of Temperature and Time on Aircraft and Missile Structures written by Stanford University. Department of Aeronautical Engineering and published by . This book was released on 1961 with total page 102 pages. Available in PDF, EPUB and Kindle. Book excerpt: A survey is made of the new problems introduced in the structural analysis of airplanes and missiles by the high temperatures caused by aerodynamic heating. Thermal stresses, thermal buckling, the effect of creep on stress distribution and stability, and ablation are discussed and special attention is paid to the behavior of the pure shells used in missiles. It is concluded that the modern structural analyst must acquire a knowledge of many disciplines that were of no interest to his predecessor working before World War II. Among these disciplines are thermodynamics, metallurgy, and the physics of the solid state. In all the new problems two parameters appear that did not enter classical structural analysis. The first is temperature which is the cause of all the difficulties of the modern structural designer and analyst. The second is time, because at high temperatures no structure can carry loads for indefinitely long periods. One of the most important tasks of the analyst of missiles is the determination of the lifetime of the structure. (Author).
Author : James Benson Preston
Publisher :
ISBN 13 :
Total Pages : 210 pages
Book Rating : 4.3/5 (91 download)
Download or read book Determination of the Mechanical Properties of Aircraft-structural Materials at Very High Temperatures After Rapid Heating written by James Benson Preston and published by . This book was released on 1958 with total page 210 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Author : Bruno A. Boley
Publisher :
ISBN 13 :
Total Pages : 44 pages
Book Rating : 4.M/5 ( download)
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:
Author : A. Clyde Willhelm
Publisher :
ISBN 13 :
Total Pages : 46 pages
Book Rating : 4.3/5 (91 download)
Download or read book Determination of the Mechanical Properties of Aircraft-structural Materials at Very High Temperatures After Rapid Heating written by A. Clyde Willhelm and published by . This book was released on 1960 with total page 46 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Author : H.F. Allen, M.A. Brull, W.J. Wilkie
Publisher :
ISBN 13 :
Total Pages : 134 pages
Book Rating : 4.3/5 (91 download)
Download or read book A study of Stress Analysis and Structural Testing Prcedures Applicable to Aircraft Structures at Elevated Temperatures written by H.F. Allen, M.A. Brull, W.J. Wilkie and published by . This book was released on 1954 with total page 134 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Author : Jeremy V. Gluck
Publisher :
ISBN 13 :
Total Pages : 104 pages
Book Rating : 4.3/5 (91 download)
Download or read book Effect of Prior Creep on Mechanical Properties of Aircraft Structural Metals written by Jeremy V. Gluck and published by . This book was released on 1958 with total page 104 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Author : Nicholas John Hoff
Publisher :
ISBN 13 :
Total Pages : 357 pages
Book Rating : 4.:/5 (859 download)
Download or read book High Temperature Effects in Aircraft Structure written by Nicholas John Hoff and published by . This book was released on 1958 with total page 357 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Author : American Society of Mechanical Engineers. Aviation and Space Division
Publisher :
ISBN 13 :
Total Pages : 188 pages
Book Rating : 4.:/5 (89 download)
Download or read book Symposium on Structures for Thermal Flight written by American Society of Mechanical Engineers. Aviation and Space Division and published by . This book was released on 1956 with total page 188 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Author : Douglas Aircraft Company
Publisher :
ISBN 13 :
Total Pages : 178 pages
Book Rating : 4.3/5 (91 download)
Download or read book Effect of Compressive Loads on Structural Fatigue at Elevated Temperature written by Douglas Aircraft Company and published by . This book was released on 1962 with total page 178 pages. Available in PDF, EPUB and Kindle. Book excerpt: The effects of compressive loads on structural fatigue at elevated temperatures are investigated using plain, notched, and welded Titanium 8Al-1Mo-1V, and PH 15-7Mo stainless steel coupon specimens. Specimens are subjected to Mach 3 spectrum test environment, including compressive loads. Fatigue life predictions are compared with spectrum teset results. The influence of prior stress-strain history on subsequent life is considered. Prediction methods are extended to include the compression range, and results notched specimens is determined analytically and experimentally. A variety of individual variable fatigue tests are performed at temperatures up to 900F.
