Author: A. M. Stagg
Publisher:
ISBN:
Category :
Languages : en
Pages : 64
Book Description
A theoretical analysis has been made of the inaccuracies involved in the representation of a continuous distribution of aircraft gust loads by a program of loads at a few discrete levels to be applied to a fatigue test specimen. These inaccuracies arise through the failure of the simplified test load program to inflict fatigue damage at the correct rate in those parts of the specimen where the stress per unit acceleration has a value other than that for which the test loading was derived. Three severities of gust spectrum and two families of S-N curve were used in the fatigue damage calculations which were based on Miner's hypothesis. The number of discrete load levels in the derived programs varied from one to seven. (Modified author abstract).
A Theoretical Study of Inaccuracies Arising from the Representation of a Continuous Gust Spectrum by a Programme of Discrete Loads in Fatigue Tests
Author: A. M. Stagg
Publisher:
ISBN:
Category :
Languages : en
Pages : 64
Book Description
A theoretical analysis has been made of the inaccuracies involved in the representation of a continuous distribution of aircraft gust loads by a program of loads at a few discrete levels to be applied to a fatigue test specimen. These inaccuracies arise through the failure of the simplified test load program to inflict fatigue damage at the correct rate in those parts of the specimen where the stress per unit acceleration has a value other than that for which the test loading was derived. Three severities of gust spectrum and two families of S-N curve were used in the fatigue damage calculations which were based on Miner's hypothesis. The number of discrete load levels in the derived programs varied from one to seven. (Modified author abstract).
Publisher:
ISBN:
Category :
Languages : en
Pages : 64
Book Description
A theoretical analysis has been made of the inaccuracies involved in the representation of a continuous distribution of aircraft gust loads by a program of loads at a few discrete levels to be applied to a fatigue test specimen. These inaccuracies arise through the failure of the simplified test load program to inflict fatigue damage at the correct rate in those parts of the specimen where the stress per unit acceleration has a value other than that for which the test loading was derived. Three severities of gust spectrum and two families of S-N curve were used in the fatigue damage calculations which were based on Miner's hypothesis. The number of discrete load levels in the derived programs varied from one to seven. (Modified author abstract).
Scientific and Technical Aerospace Reports
AGARD Advisory Report
Aeronautical Engineering
Author:
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 520
Book Description
A selection of annotated references to unclassified reports and journal articles that were introduced into the NASA scientific and technical information system and announced in Scientific and technical aerospace reports (STAR) and International aerospace abstracts (IAA)
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 520
Book Description
A selection of annotated references to unclassified reports and journal articles that were introduced into the NASA scientific and technical information system and announced in Scientific and technical aerospace reports (STAR) and International aerospace abstracts (IAA)
BLLD Announcement Bulletin
Author: British Library. Lending Division
Publisher:
ISBN:
Category : Science
Languages : en
Pages : 592
Book Description
Publisher:
ISBN:
Category : Science
Languages : en
Pages : 592
Book Description
Government Reports Index
Author:
Publisher:
ISBN:
Category : Government publications
Languages : en
Pages : 1262
Book Description
Publisher:
ISBN:
Category : Government publications
Languages : en
Pages : 1262
Book Description
Government Reports Announcements
Government Reports Annual Index
Author:
Publisher:
ISBN:
Category : Government reports announcements & index
Languages : en
Pages : 872
Book Description
Publisher:
ISBN:
Category : Government reports announcements & index
Languages : en
Pages : 872
Book Description
Government Reports Announcements & Index
Full-scale Fatigue Testing of Aircraft Structures
Author: Frederik Johan Plantema
Publisher:
ISBN:
Category : Airframes
Languages : en
Pages : 444
Book Description
Publisher:
ISBN:
Category : Airframes
Languages : en
Pages : 444
Book Description