Index of NACA Technical Publications
Author : United States. National Advisory Committee for Aeronautics
Publisher :
Page : 616 pages
File Size : 45,17 MB
Release : 1949
Category : Aeronautics
ISBN :
Author : United States. National Advisory Committee for Aeronautics
Publisher :
Page : 616 pages
File Size : 45,17 MB
Release : 1949
Category : Aeronautics
ISBN :
Author : Pai C. Hu
Publisher :
Page : 544 pages
File Size : 17,61 MB
Release : 1946
Category : Buckling (Mechanics)
ISBN :
(3) The Southwell plot method of predicting theoretical critical stresses for perfect specimens from experimental observations on actual specimens may not be expected to give, in general, satisfactory results when applied to flat plates.
Author : United States. National Advisory Committee for Aeronautics
Publisher :
Page : 916 pages
File Size : 20,67 MB
Release : 1946
Category : Aeronautics
ISBN :
Author : United States. Department of Defense
Publisher :
Page : 382 pages
File Size : 17,80 MB
Release : 1961
Category : Airplanes
ISBN :
Author : United States. ANC-5 Panel on Strength of Metal Aircraft Elements
Publisher :
Page : 200 pages
File Size : 10,53 MB
Release : 1955
Category : Airplanes
ISBN :
Author :
Publisher :
Page : 664 pages
File Size : 18,57 MB
Release : 1949
Category : Aeronautics
ISBN :
Author : United States. Munitions Board. Aircraft Committee. Subcommittee on Air Force-Navy-Civil Aircraft Design Criteria
Publisher :
Page : 202 pages
File Size : 14,23 MB
Release : 1955
Category : Airplanes
ISBN :
Author : Michael R. Urban Ph.D.
Publisher : Covenant Books, Inc.
Page : 121 pages
File Size : 44,30 MB
Release : 2023-10-02
Category : Technology & Engineering
ISBN :
Accounting for fatigue loadings has been a concern ever since the widespread introduction of metallic materials into load-bearing components in the nineteenth century. Calculations were developed based on the analysis capabilities of their time incorporating all the latest technologies of their era. At the time, that technology was pencil-and-paper calculations. Today's calculations are computer-based. The widespread use of computing methods has greatly enhanced the analyst abilities for simulating internal stress and strain fields. Unfortunately, current fatigue analyses often force-fit current stress field calculations into fatigue analysis methods meant for nineteenth century stress calculation methods. It's never a good idea to force methods optimized for pre-computer calculations to work with computers. This text presents a more integrated approach to computer-based fatigue analysis methods. Like what was originally done, the latest technologies are applied rather than force-fitting computer computational capabilities into nineteenth-century techniques. Holistic approaches incorporating all knowledge have long been established as the most successful approach to problem-solving. Incorporating all knowledge with the most modern capabilities is the preferred approach. Holistic methods strive to reduce subjective inputs and replace them with consistent objective ones. This text aims to transition disjointed inefficient analyses into a unified computer-based holistic technique by introducing a fatigue analysis method specifically developed for computer simulations. Ultimately, for any method or theory to be valuable, it must be put into practice and prove itself. That entails leadership decision-making. Engineering design development activities will lead to final decisions. Information in a holistic approach must include the reliability of the information. How consistent are the predictions? Are the two types of potential scatter, analytic, and physical properly addressed? Is analytic scatter minimized while maintaining creativity? Is physical scatter totally understood? Effective program management requires knowledge on both types of scatter and, most importantly, the ability to realize the difference. A novel computer-based unified approach to fatigue methods is presented which incorporates a holistic approach for more accurate and consistent analyses, including the management and leadership of fatigue analysis projects, minimization of analytic scatter, management of physical scatter, and unification of methods that minimize subjective inputs often needed to bridge inconsistent techniques.
Author : United States. Department of Defense
Publisher :
Page : 820 pages
File Size : 22,93 MB
Release : 1966
Category : Airplanes
ISBN :
Author : W. Weibull
Publisher : Elsevier
Page : 322 pages
File Size : 35,32 MB
Release : 2013-10-22
Category : Technology & Engineering
ISBN : 1483154165
Fatigue Testing and Analysis of Results discusses fundamental concepts of fatigue testing and results analysis. The book begins with a description of the symbols and nomenclature selected for the present book, mainly those proposed by the ASTM Committee E-9 on Fatigue. Fatigue testing methods are then discussed including routine tests, short-life and long-life tests, cumulative-damage tests, and abbreviated and accelerated tests. Separate chapters cover fatigue testing machines and equipment; instruments and measuring devices; and test pieces used in fatigue testing. The factors affecting test results are considered, including material, types of stressing, test machine, environment, and testing technique. The final two chapters cover the planning of test programs and the presentation of results. Test program planning involves the statistical design of a test series; specification and sampling of test pieces; and choice of test pieces, testing machines, and test conditions. The chief purpose of most fatigue tests is the experimental determination of the relation between the endurance and the magnitude of the applied stress range for the material and the specimen under consideration, and final results can be condensed into a table, graph, or analytical expression.