Author: Dean R. Chapman
Publisher:
ISBN:
Category : Aerofoils
Languages : en
Pages : 206
Book Description
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
Author: Dean R. Chapman
Publisher:
ISBN:
Category : Aerofoils
Languages : en
Pages : 206
Book Description
Publisher:
ISBN:
Category : Aerofoils
Languages : en
Pages : 206
Book Description
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
Author: Lewis R. Fisher
Publisher:
ISBN:
Category :
Languages : en
Pages : 27
Book Description
Publisher:
ISBN:
Category :
Languages : en
Pages : 27
Book Description
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
Author: Lewis R. Fisher
Publisher:
ISBN:
Category : Airplanes
Languages : en
Pages : 0
Book Description
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.
Publisher:
ISBN:
Category : Airplanes
Languages : en
Pages : 0
Book Description
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 Effects of Frequency and Amplitude on the Lateral Stability Derivatives for a Delta, a Swept, and an Upswept Wing Oscillating in Yaw
Author: Lewis R. Fisher
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 27
Book Description
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 27
Book Description
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
Author: Lewis R. Fisher
Publisher:
ISBN:
Category : Airplanes
Languages : en
Pages : 67
Book Description
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.
Publisher:
ISBN:
Category : Airplanes
Languages : en
Pages : 67
Book Description
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 of Oscillation on the Roll-stability Derivatives for a 60 Degree Delta-wing Airplane Model
Author: Lewis R. Fisher
Publisher:
ISBN:
Category : Vibration
Languages : en
Pages : 58
Book Description
Publisher:
ISBN:
Category : Vibration
Languages : en
Pages : 58
Book Description
Analysis of the Dynamic Lateral Stability of a Delta-wing Airplane with Frequency-dependent Stability Derivatives
Author: Albert E. Brown
Publisher:
ISBN:
Category : Aerodynamics
Languages : en
Pages : 48
Book Description
Publisher:
ISBN:
Category : Aerodynamics
Languages : en
Pages : 48
Book Description
USAF Stability and Control Datcom
Author: Douglas Aircraft Company
Publisher:
ISBN:
Category : Airplanes
Languages : en
Pages : 684
Book Description
Publisher:
ISBN:
Category : Airplanes
Languages : en
Pages : 684
Book Description
Experimental Determination of the Effects of Frequency and Amplitude of Oscillation on the Roll-stability Derivatives for a 60° Delta-wing Airplane Model
Author: Lewis R. Fisher
Publisher:
ISBN:
Category :
Languages : en
Pages : 0
Book Description
Publisher:
ISBN:
Category :
Languages : en
Pages : 0
Book Description
Experimental Determination of the Effects of Frequency and Amplitude of Oscillation on the Roll-stability Derivatives for a 60 Degree Delta-wing Airplane Model
Author: Lewis R. Fisher
Publisher:
ISBN:
Category :
Languages : en
Pages : 0
Book Description
Publisher:
ISBN:
Category :
Languages : en
Pages : 0
Book Description