Author: Jens Rainier Maria Radok
Publisher:
ISBN:
Category :
Languages : en
Pages : 48
Book Description
The Problem of Gust Loads on Aircraft: a Survey of the Theoretical Treatment
Author: Jens Rainier Maria Radok
Publisher:
ISBN:
Category :
Languages : en
Pages : 48
Book Description
Publisher:
ISBN:
Category :
Languages : en
Pages : 48
Book Description
Gust Loads on Aircraft
Author: Frederic M. Hoblit
Publisher: AIAA
ISBN: 9781600860607
Category : Airplanes
Languages : en
Pages : 332
Book Description
Publisher: AIAA
ISBN: 9781600860607
Category : Airplanes
Languages : en
Pages : 332
Book Description
Structural Response to Discrete and Continuous Gusts of an Airplane Having Wing-bending Flexibility and a Correlation of Calculated and Flight Results
Author: Antonio Ferri
Publisher:
ISBN:
Category : Aerodynamic load
Languages : en
Pages : 278
Book Description
Publisher:
ISBN:
Category : Aerodynamic load
Languages : en
Pages : 278
Book Description
A Study of the Aircraft Gust Loads Problem and Recommendations for a Flight Research Investigation
Author: Lawrence Beatty Reynolds
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 74
Book Description
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 74
Book Description
An Introduction to the Theory of Aeroelasticity
Author: Y C Fung
Publisher: Courier Dover Publications
ISBN: 0486469360
Category : Technology & Engineering
Languages : en
Pages : 516
Book Description
Geared toward advanced undergraduates and graduate students, this outstanding text surveys aeroelastic problems, their historical background, basic physical concepts, and the principles of analysis.
Publisher: Courier Dover Publications
ISBN: 0486469360
Category : Technology & Engineering
Languages : en
Pages : 516
Book Description
Geared toward advanced undergraduates and graduate students, this outstanding text surveys aeroelastic problems, their historical background, basic physical concepts, and the principles of analysis.
The Application of the Statistical Theory of Extreme Values to Gust-load Problems
Author: Harry Press
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 50
Book Description
This paper contains an analysis of the applicability of the statistical theory of extreme values to the problems of predicting the frequency of encountering the larger gust loads and velocities in flight through rough air. The results indicate that the distribution of maximum values of gust loads and velocities, under both test conditions and in normal commercial transport operations, may be represented by a simple analytic form. Methods of application and methods of measuring the reliability of the estimates are also given.
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 50
Book Description
This paper contains an analysis of the applicability of the statistical theory of extreme values to the problems of predicting the frequency of encountering the larger gust loads and velocities in flight through rough air. The results indicate that the distribution of maximum values of gust loads and velocities, under both test conditions and in normal commercial transport operations, may be represented by a simple analytic form. Methods of application and methods of measuring the reliability of the estimates are also given.
Report
Report
Author: United States. National Advisory Committee for Aeronautics
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 32
Book Description
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 32
Book Description
Technical Note - National Advisory Committee for Aeronautics
Author: United States. National Advisory Committee for Aeronautics
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 802
Book Description
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 802
Book Description
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).