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

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 Author: Dean R. Chapman
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ISBN:
Category : Aerofoils
Languages : en
Pages : 206

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Experimental Determination of Effects of Frequency and Amplitude on the Lateral Stability Derivatives for a Delta, a Swept, and an Unswept Wing Oscillating in Yaw

Experimental Determination of Effects of Frequency and Amplitude on the Lateral Stability Derivatives for a Delta, a Swept, and an Unswept Wing Oscillating in Yaw PDF Author: Lewis R. Fisher
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Category :
Languages : en
Pages : 27

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Experimental Determination of the Effects of Frequency and Amplitude of Oscillation on the Roll-stability Derivatives for a 60© Delta-wing Airplane Model

Experimental Determination of the Effects of Frequency and Amplitude of Oscillation on the Roll-stability Derivatives for a 60© Delta-wing Airplane Model PDF Author: Lewis R. Fisher
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Category : Airplanes
Languages : en
Pages : 54

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Experimental Determination of the Effects of Frequency and Amplitude of Oscillation on the Roll-stability Derivatives for a 60 Degree Delta-wing Airplane Model

Experimental Determination of the Effects of Frequency and Amplitude of Oscillation on the Roll-stability Derivatives for a 60 Degree Delta-wing Airplane Model PDF Author: Lewis R. Fisher
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ISBN:
Category : Vibration
Languages : en
Pages : 54

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Experimental Determination of the Effects of Frequency and Amplitude on the Lateral Stability Derivatives for a Delta, a Swept, and an Unswept Wing Oscillating in Yaw

Experimental Determination of the Effects of Frequency and Amplitude on the Lateral Stability Derivatives for a Delta, a Swept, and an Unswept Wing Oscillating in Yaw PDF Author: Lewis R. Fisher
Publisher:
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.

Experimental Determination of the Effects of Frequency and Amplitude on the Lateral Stability Derivatives for a Delta, a Swept, and an Unswept Wing Oscillating in Yaw

Experimental Determination of the Effects of Frequency and Amplitude on the Lateral Stability Derivatives for a Delta, a Swept, and an Unswept Wing Oscillating in Yaw PDF 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.

Index of NASA Technical Publications

Index of NASA Technical Publications PDF Author: United States. National Aeronautics and Space Administration
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ISBN:
Category : Aeronautics
Languages : en
Pages : 500

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NASA Technical Memorandum

NASA Technical Memorandum PDF Author:
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ISBN:
Category : Aeronautics
Languages : en
Pages : 592

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Technical Note - National Advisory Committee for Aeronautics

Technical Note - National Advisory Committee for Aeronautics PDF Author: United States. National Advisory Committee for Aeronautics
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Category : Aeronautics
Languages : en
Pages : 378

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Rate of Reaction of Gaseous Fluorine with Water Vapor at 35 Degrees C

Rate of Reaction of Gaseous Fluorine with Water Vapor at 35 Degrees C PDF Author: Vernon A. Slabey
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Category : Chemical kinetics
Languages : en
Pages : 678

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Book Description
Fluorine and water vapor react extremely slowly or not at all in the gas phase at 35 degrees C at partial pressures of the reactants up to 40 mm of mercury. They react at surfaces; the kinetics are first order with respect to each of the reactants.