Effect of Automatic Stabilization on the Lateral Oscillatory Stability of a Hypothetical Airplane at Supersonic Speeds PDF Download
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Author: Leonard Sternfield
Publisher:
ISBN:
Category : Aerodynamics, Supersonic
Languages : en
Pages : 698
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Book Description
(1) an automatic pilot sensitive to either a displacement in yaw or roll.
Author: Leonard Sternfield
Publisher:
ISBN:
Category : Aerodynamics, Supersonic
Languages : en
Pages : 698
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Book Description
(1) an automatic pilot sensitive to either a displacement in yaw or roll.
Author: United States. National Advisory Committee for Aeronautics
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 440
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Book Description
Author: United States. National Advisory Committee for Aeronautics
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 944
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Book Description
Author: Robert O. Schade
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 66
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Book Description
The results of an experimental and theoretical investigation of the effects of large artificial variations of four rotary stability derivatives on the dynamic lateral stability and control of a 45 degree sweptback-wing airplane model are presented. The experimental results are presented mainly in the form of flight ratings for stability, control, and general flight behavior. Calculations of period and damping and of the response of rolling and yawing disturbances are also presented.
Author: Jerome B. Hammack
Publisher:
ISBN:
Category : Aerodynamics, Supersonic
Languages : en
Pages : 682
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Book Description
The aerodynamic design of propellers from considerations of centrifugal force is presented. A solution is obtained for the span wise distribution of cross-sectional area required to attain constant centrifugal stress over most of the blade.
Author: Leonard Sternfield
Publisher:
ISBN:
Category : Airplanes
Languages : en
Pages : 36
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Book Description
A method is presented for determining the effect of time lag in an automatic stabilization system on the lateral oscillatory stability of an airplane. The method is applied to a typical present-day airplane equipped with an automatic pilot sensitive to yawing acceleration and geared to the rudder so that rudder control is application in proportion to the yawing acceleration.
Author: United States. National Advisory Committee for Aeronautics
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 702
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Book Description
Author: United States. National Advisory Committee for Aeronautics
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages :
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Book Description
Includes the Committee's Technical reports no. 1-1058, reprinted in v. 1-37.
Author: United States. National Advisory Committee for Aeronautics
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 36
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Book Description
Author:
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 664
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Book Description
