Matrix Method of Determining the Longitudinal-stability Coefficients and Frequency Response of an Aircraft from Transient Flight Data PDF Download
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Author: James J. Donegan
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 40
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Book Description
A method is presented for obtaining the over-all longitudinal-stability coefficients and frequency response of an aircraft from an analysis of arbitrary maneuvers in which simple instrumentation is used. Although the method presented deals entirely with the aircraft, it is equally applicable to other problems which can be expressed by second-order differential equations.
Author: James J. Donegan
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 40
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Book Description
A method is presented for obtaining the over-all longitudinal-stability coefficients and frequency response of an aircraft from an analysis of arbitrary maneuvers in which simple instrumentation is used. Although the method presented deals entirely with the aircraft, it is equally applicable to other problems which can be expressed by second-order differential equations.
Author: United States. National Advisory Committee for Aeronautics
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 22
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Author:
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 900
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Author: United States. National Advisory Committee for Aeronautics
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages :
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Includes the Committee's Technical reports no. 1-1058, reprinted in v. 1-37.
Author:
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 750
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Author: United States. National Advisory Committee for Aeronautics
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 274
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Author: Vernon H. Gray
Publisher:
ISBN:
Category : Aerofoils
Languages : en
Pages : 720
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Book Description
The effects of primary and runback icing and frost formations on the drag of an 8-foot-chord NACA 651-212 airfoil section were investigated over a range of angles of attack from 2 degrees to 8 degrees and airspeeds up to 260 miles per hour for icing conditions with liquid-water contents ranging from 0.25 to 1.4 grams per cubic meter and datum air temperatures of -30 to 30 degrees F.
Author: United States. National Advisory Committee for Aeronautics
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 992
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Author: Lloyd Eugene Wilkie
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 164
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Author: Aaron S. Boksenbom
Publisher:
ISBN:
Category : Aerofoils
Languages : en
Pages : 226
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