Experimental Determination of Effects of Frequency and Amplitude on the Lateral Stability Derivatives for a Delta, a Swept, and an Upswept Wing Oscillating in Yaw PDF Download
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Author: Dean R. Chapman
Publisher:
ISBN:
Category : Aerofoils
Languages : en
Pages : 206
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Author: Dean R. Chapman
Publisher:
ISBN:
Category : Aerofoils
Languages : en
Pages : 206
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Author: Lewis R. Fisher
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Category :
Languages : en
Pages : 27
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Author: Lewis R. Fisher
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ISBN:
Category : Airplanes
Languages : en
Pages : 54
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Author: Lewis R. Fisher
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Category : Vibration
Languages : en
Pages : 54
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Author: Lewis R. Fisher
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ISBN:
Category : Airplanes
Languages : en
Pages : 0
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Effects of amplitude of oscillation on the stability derivatives for the delta wing were evident for certain high angles of attack and for the lowest frequencies of oscillation. As the frequency became high, the amplitude effects tended to disappear.
Author: Lewis R. Fisher
Publisher:
ISBN:
Category : Airplanes
Languages : en
Pages : 67
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Effects of amplitude of oscillation on the stability derivatives for the delta wing were evident for certain high angles of attack and for the lowest frequencies of oscillation. As the frequency became high, the amplitude effects tended to disappear.
Author: United States. National Aeronautics and Space Administration
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ISBN:
Category : Aeronautics
Languages : en
Pages : 384
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Author: United States. National Advisory Committee for Aeronautics
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ISBN:
Category : Aeronautics
Languages : en
Pages : 388
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Author: United States. National Aeronautics and Space Administration
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Category :
Languages : en
Pages : 208
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Author:
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Category : Aeronautics
Languages : en
Pages : 818
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