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Author:
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ISBN:
Category : Aeronautics
Languages : en
Pages : 1196
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Author:
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 1196
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Book Description
Author: Frank A. DuWaldt
Publisher:
ISBN:
Category : Flutter (Aerodynamics)
Languages : en
Pages : 326
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Author:
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 732
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Book Description
Author: United States. National Advisory Committee for Aeronautics
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 1142
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Author: Harry H. Heyson
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ISBN:
Category : Air flow
Languages : en
Pages : 696
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Book Description
Results of an investigation in the Langley full-scale tunnel of the induced flow near a lifting rotor are given. Measurements of stream angles and velocities were made in several transverse planes along and behind the rotor in four different conditions representative of the cruising and high-speed ranges of flight. These measurements indicate that available theory may be used to calculate with reasonable accuracy the induced flow over the forward three-quarters of the disk for these flight conditions provided that a realistic nonuniform rotor disk-load distribution is assumed. Rearward of the three-quarter-diameter point, calculations of the induced velocity are increasingly inaccurate due to the rolling up of the trailing-vortex system. Farther rearward, well behind the rotor, the flow may be represented more accurately by the flow behind a uniformly loaded wing.
Author:
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 900
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Book Description
Author: United States. National Advisory Committee for Aeronautics
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 100
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Author: United States. National Advisory Committee for Aeronautics
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 580
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Author:
Publisher:
ISBN:
Category : Aerodynamic load
Languages : en
Pages : 606
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Author:
Publisher:
ISBN:
Category : Mechanics, Applied
Languages : en
Pages : 616
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Book Description
