A Flight Investigation of the Thermal Performance of an Air-heated Propeller PDF Download
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Author: John F. Darsow
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 568
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Book Description
The thermal performance of an air-heated propeller, installed on a test airplane, was evaluated by observations of the ice-prevention propertiesof the propeller during flight in natural-icing conditions and by the collection of thermal data on the propeller during flight in clear air and in clouds at temperatures above freezing. The test propeller was equipped with hollow steel blades of a standard design which were altered to permit heated air to enter the blade cavities at the propeller hub and to leave the cavities at the blade tips. No provisions were made to control the distribution of air flow inside the blades.
Author: John F. Darsow
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 568
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Book Description
The thermal performance of an air-heated propeller, installed on a test airplane, was evaluated by observations of the ice-prevention propertiesof the propeller during flight in natural-icing conditions and by the collection of thermal data on the propeller during flight in clear air and in clouds at temperatures above freezing. The test propeller was equipped with hollow steel blades of a standard design which were altered to permit heated air to enter the blade cavities at the propeller hub and to leave the cavities at the blade tips. No provisions were made to control the distribution of air flow inside the blades.
Author: Lewis A. Rodert
Publisher:
ISBN:
Category : Airplanes
Languages : en
Pages : 26
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Book Description
The thermal properties are presented for the exhaust heated wing de-icing system of a Lockheed 12-A airplane which has successfully prevented wing icing in 25 hours of flying in various icing conditions. The quantities of heat supplied for de-icing of the wings under various conditions were measured and are presented. The distribution of temperatures above the ambient air temperature for the wing surface under various operating conditions are given. The design and construction factors relative to the weight, maintenance, and the applicability to exhaust heating on other airplanes are discussed.
Author: United States. National Advisory Committee for Aeronautics
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 162
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Author: United States. National Advisory Committee for Aeronautics
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 616
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Author:
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 664
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Author: United States. National Advisory Committee for Aeronautics
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 994
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Author:
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 1908
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Author:
Publisher:
ISBN:
Category : Government publications
Languages : en
Pages : 1860
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Book Description
Author:
Publisher:
ISBN:
Category : Government publications
Languages : en
Pages :
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Author: United States. National Advisory Committee for Aeronautics
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 516
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Book Description
