The Relation Between Spanwise Variations in the Critical Mach Number and Spanwise Load Distributions PDF Download
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Author: Richard T. Whitcomb
Publisher:
ISBN:
Category : Aerodynamic load
Languages : en
Pages : 12
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Book Description
Summary: Data are presented to show the changes that occur in the spanwise load distributions on wings when the critical Mach number is exceeded. These data indicate that the magnitude of the changes in spanwise load distribution varies with the magnitude of the spanwise variation in the critical Mach numbers of the sections. Means of reducing the magnitudes of such changes are considered.
Author: Richard T. Whitcomb
Publisher:
ISBN:
Category : Aerodynamic load
Languages : en
Pages : 12
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Book Description
Summary: Data are presented to show the changes that occur in the spanwise load distributions on wings when the critical Mach number is exceeded. These data indicate that the magnitude of the changes in spanwise load distribution varies with the magnitude of the spanwise variation in the critical Mach numbers of the sections. Means of reducing the magnitudes of such changes are considered.
Author:
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 762
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Book Description
Reproductions of reports, some declassified, of research done at Langley Memorial Aeronautical Laboratory during World War II. The order of reports does not represent when they were chronologically issued. Reference to the original version of each report is included.
Author: United States. National Advisory Committee for Aeronautics
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 298
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Book Description
Author:
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 316
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Book Description
Author: United States. National Advisory Committee for Aeronautics
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 692
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Book Description
Author: United States. National Advisory Committee for Aeronautics
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 1146
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Book Description
Author: F. E. West
Publisher:
ISBN:
Category : Aerofoils
Languages : en
Pages : 56
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Book Description
The effects of compressibility on the lift, pressure, pitching-moment, and load characteristics of a 12-foot tapered wing having NACA 64-210 airfoil sections and aspect ratio of 6 is presented for Mach numbers up to 0.60 and an angle-of-attack range of -4 degrees up through the stall.
Author: United States. National Advisory Committee for Aeronautics
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 758
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Book Description
Author:
Publisher:
ISBN:
Category : Science
Languages : en
Pages : 86
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Book Description
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.
