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Author : Dwight O. Fearnow
Publisher :
ISBN 13 :
Total Pages : 34 pages
Book Rating : 4.3/5 (91 download)
Download or read book Investigation of the Fatigue Strength of a Full-scale Airplane Wing Structures written by Dwight O. Fearnow and published by . This book was released on 1951 with total page 34 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Author : M. James McGuigan
Publisher :
ISBN 13 :
Total Pages : 36 pages
Book Rating : 4.:/5 (669 download)
Download or read book Interim Report on a Fatigue Investigation of a Full-scale Transport Aircraft Wing Structure written by M. James McGuigan and published by . This book was released on 1953 with total page 36 pages. Available in PDF, EPUB and Kindle. Book excerpt: Results are presented of an investigation of the fatigue strength of several full-scale aircraft wing structures. The test specimens wre obtained from C-46 "Commando" type airpales and the tests described are the first phase of a larger research program on the fatigue strength of full-scale aircraft. The tests were conducted by the resonant-frequency method at a level of 1 plus or minus 0.625 h or about 22 plus or minus 14 percent of the design ultimate load factor.
Author : Frederik Johan Plantema
Publisher :
ISBN 13 :
Total Pages : 444 pages
Book Rating : 4.:/5 (41 download)
Download or read book Full-scale Fatigue Testing of Aircraft Structures written by Frederik Johan Plantema and published by . This book was released on 1961 with total page 444 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Author : United States. Naval Air Systems Command
Publisher :
ISBN 13 :
Total Pages : 360 pages
Book Rating : 4.F/5 ( download)
Download or read book Fatigue of Aircraft Structures written by United States. Naval Air Systems Command and published by . This book was released on 1966 with total page 360 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Author :
Publisher : ASTM International
ISBN 13 :
Total Pages : 275 pages
Book Rating : 4./5 ( download)
Download or read book Symposium on Fatigue Tests of Aircraft Structures: Low-Cycle, Full-Scale, and Helicopters written by and published by ASTM International. This book was released on 1963 with total page 275 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Author : Lee R. Foster
Publisher :
ISBN 13 :
Total Pages : 42 pages
Book Rating : 4.:/5 (31 download)
Download or read book Fatigue Investigation of Full-scale Transport-airplane Wings written by Lee R. Foster and published by . This book was released on 1960 with total page 42 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Author : W. Barrois
Publisher :
ISBN 13 :
Total Pages : 380 pages
Book Rating : 4.E/5 ( download)
Download or read book Fatigue of Aircraft Structures written by W. Barrois and published by . This book was released on 1963 with total page 380 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Author : United States. National Advisory Committee for Aeronautics
Publisher :
ISBN 13 :
Total Pages : 1034 pages
Book Rating : 4.E/5 ( download)
Download or read book Technical Note - National Advisory Committee for Aeronautics written by United States. National Advisory Committee for Aeronautics and published by . This book was released on 1953 with total page 1034 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Author : Harry Bernstein
Publisher :
ISBN 13 :
Total Pages : 686 pages
Book Rating : 4.F/5 ( download)
Download or read book Effects of Parallel-jet Mixing on Downstream Mach Number and Stagnation Pressure with Application to Engine Testing in Supersonic Tunnels written by Harry Bernstein and published by . This book was released on 1953 with total page 686 pages. Available in PDF, EPUB and Kindle. Book excerpt: A one-dimensional analysis of the results of the parallel-jet mixing encountered in the testing of engines in supersonic wind tunnels is reported. Equations were derived for determining the total pressure and Mach number behind the tunnel terminal shock. The method represents a simple procedure for determining these quantities while a tunnel is still in the design stage. A specific example of the method is included.
Author : Richard E. Whaley
Publisher :
ISBN 13 :
Total Pages : 43 pages
Book Rating : 4.:/5 (249 download)
Download or read book Fatigue Investigation of Full-scale Transport-airplane Wings written by Richard E. Whaley and published by . This book was released on 1957 with total page 43 pages. Available in PDF, EPUB and Kindle. Book excerpt: This report included results of simulated flight-history tests which are part of a program on the fatigue strength of the wings of C-46 airplanes. The tests were conducted by the forced-vibration method, in which a spectrum of loads derived from gust-frequency statistics was used. The results are compared with the previously published results of constant-amplitude fatigue tests.
Author : United States. National Advisory Committee for Aeronautics
Publisher :
ISBN 13 :
Total Pages : 10 pages
Book Rating : 4.3/5 (126 download)
Download or read book Research Abstracts written by United States. National Advisory Committee for Aeronautics and published by . This book was released on 1951 with total page 10 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Author : United States. National Advisory Committee for Aeronautics
Publisher :
ISBN 13 :
Total Pages : 388 pages
Book Rating : 4.:/5 (2 download)
Download or read book Index of NACA Technical Publications written by United States. National Advisory Committee for Aeronautics and published by . This book was released on 1959 with total page 388 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Author :
Publisher :
ISBN 13 :
Total Pages : 750 pages
Book Rating : 4.X/5 (4 download)
Download or read book A Selected Listing of NASA Scientific and Technical Reports for ... written by and published by . This book was released on 1949 with total page 750 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Author : Claude B. Castle
Publisher :
ISBN 13 :
Total Pages : 38 pages
Book Rating : 4.:/5 (31 download)
Download or read book Fatigue Investigation of Full-scale Wing Panels of 7075 Aluminum Alloy written by Claude B. Castle and published by . This book was released on 1961 with total page 38 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Author : E. Gassner
Publisher : Elsevier
ISBN 13 : 1483185818
Total Pages : 535 pages
Book Rating : 4.4/5 (831 download)
Download or read book Fatigue Design Procedures written by E. Gassner and published by Elsevier. This book was released on 2014-05-16 with total page 535 pages. Available in PDF, EPUB and Kindle. Book excerpt: Fatigue Design Procedures presents the full text of the papers presented at the 4th Symposium of the International Committee on Aeronautical Fatigue held in Munich, Germany on June 16-18, 1965, and summaries of the discussion held about them. The papers featured in the volume covers different aspects of fatigue design. These include fail-safe design for a jet transport airplane, the weapon systems fatigue certification program of the U.S. Air Force, the role of variable amplitude or constant amplitude tests in design studies, the evaluation of allowable design stress and corresponding fatigue life, and the importance of fatigue design testing. This book will be of interest to persons dealing with studies on fatigue design methods.
Author : American Society for Testing Materials
Publisher :
ISBN 13 :
Total Pages : 108 pages
Book Rating : 4.3/5 (91 download)
Download or read book Fatigue of Aircraft Structures written by American Society for Testing Materials and published by . This book was released on 1957 with total page 108 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Author : A. R. Vollmecke
Publisher :
ISBN 13 :
Total Pages : 9 pages
Book Rating : 4.:/5 (125 download)
Download or read book Full Scale Wing Fatigue Testing written by A. R. Vollmecke and published by . This book was released on 1957 with total page 9 pages. Available in PDF, EPUB and Kindle. Book excerpt: The problem of fatigue in aircraft structures has been under investigation for many years. Much work has been accomplished in testing and evaluating the effects of different cyclic loads primarily upon material coupons, typical joints, and small component parts. Although this type of testing, along with service experience, has established the basis of present-day fatigue knowledge, it does not reproduce the complex load conditions that exist in a full scale aircraft structure. Only in testing of a complete aircraft structure for a given condition can the life relationship of the assembled parts and the influence of these parts on adjoining structure be determined. In recent years, limited repeated load testing of large structures has been accomplished by the use of two test methods: (1) single mass, cantilever, resonate beam type tests, and (2) distributed load application using tension pads and whiffle trees with hydraulic loading cylinders. The single mass resonate cantilever beam type test is simple in setup. A single mass placed on a wing is resonated to give the desired loading. The cyclic rate is fast, dependent only on the resonate frequency of the system. The single concentrated load however imposes a serious limitation to the testing in that the bending moment and shear produced are correct for a given condition at only one spanwise station. Torsion is generally neglected.
