A Probability Analysis of the Meteorological Factors Conducive to Aircraft Icing in the United States PDF Download
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Author: William Lewis
Publisher:
ISBN:
Category :
Languages : en
Pages : 0
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Book Description
Meteorological icing data obtained in flight in the United States are analyzed statistically and methods are developed for the determination of: (1) the various simultaneous combinations of the three basic icing parameters (liquid-water content, drop diameter, and temperature) which would have equal probability of being exceeded in flight in any random icing encounter; and (2) the probability of exceeding any specified group of values of liquid-water content associated simultaneously with temperature and drop-diameter values lying within specified ranges. The methods are particularly useful in the design of anti-icing equipment intended to operate through the United States, to define simultaneous combinations of the meteorological variables which could be encountered, and to ascertain the effectiveness of the equipment in withstanding the natural icing conditions to which it may be subjected. In addition, a mathematical basis is provided for the future statistical analysis of meteorological icing data that might be obtained throughout the world.
Author: William Lewis
Publisher:
ISBN:
Category :
Languages : en
Pages : 0
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Book Description
Meteorological icing data obtained in flight in the United States are analyzed statistically and methods are developed for the determination of: (1) the various simultaneous combinations of the three basic icing parameters (liquid-water content, drop diameter, and temperature) which would have equal probability of being exceeded in flight in any random icing encounter; and (2) the probability of exceeding any specified group of values of liquid-water content associated simultaneously with temperature and drop-diameter values lying within specified ranges. The methods are particularly useful in the design of anti-icing equipment intended to operate through the United States, to define simultaneous combinations of the meteorological variables which could be encountered, and to ascertain the effectiveness of the equipment in withstanding the natural icing conditions to which it may be subjected. In addition, a mathematical basis is provided for the future statistical analysis of meteorological icing data that might be obtained throughout the world.
Author: William Lewis
Publisher:
ISBN:
Category :
Languages : en
Pages : 93
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Book Description
Author: William Lewis
Publisher:
ISBN:
Category : Airplanes
Languages : en
Pages : 93
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Book Description
Meteorological icing data obtained in flight in the United States are analyzed statistically the methods are developed for the determination of (1) the various simultaneous combinations of the three basic icing parameters (liquid-water content, drop diameter, and temperature) which would have equal probability of being exceeded in flight in any random icing encounter, and (2) the probability of exceeding any specified group of values of liquid-water content associated simultaneously with temperature and drop-diameter values lying within specified ranges.
Author: James P. Lewis
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 24
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Book Description
Author: United States. National Advisory Committee for Aeronautics
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 312
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Book Description
Author: United States. National Advisory Committee for Aeronautics
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 614
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Book Description
Author: United States. Federal Aviation Administration
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 60
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Book Description
Author:
Publisher:
ISBN:
Category : Aerodynamics
Languages : en
Pages : 50
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Book Description
Author: United States. National Aeronautics and Space Administration
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 506
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Book Description
Author: Alton P. Mayo
Publisher:
ISBN:
Category : Bending
Languages : en
Pages : 632
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Book Description
A matrix solution for the spanwise bending moments and deflections of a torsionally rigid rotor blade subjected to an arbitrary loading is presented. The method includes the cantilever, teetering, and hinged blades in hovering and in steady forward flight. The method is comparatively short, involves only standard matrix procedures, and does not require that the mode shapes or natural frequencies be known.
