Author: M. Leroy Spearman
Publisher:
ISBN:
Category :
Languages : en
Pages : 51
Book Description
Longitudinal and Lateral Stability and Control Characteristics at Mach Number 2.01 of a 60 Degree Delta-wing Airplane Configuration Equipped with a Canard Control and with Wing Trailing-edge Flap Controls
Author: M. Leroy Spearman
Publisher:
ISBN:
Category :
Languages : en
Pages : 51
Book Description
Publisher:
ISBN:
Category :
Languages : en
Pages : 51
Book Description
Effects of Wing Height on the Stability and Control Characteristics at a Mach Number of 2.01 of a Canard Airplane Configuration with a 70 Deg Delta Wing
Author:
Publisher:
ISBN:
Category :
Languages : en
Pages : 36
Book Description
Publisher:
ISBN:
Category :
Languages : en
Pages : 36
Book Description
Longitudinal Stability and Control Characteristics at Mach Numbers from 0.70 to 2.22 of a Triangular Wing Configuration Equipped with a Canard Control, a Trailing-edge-flap Control, Or a Cambered Forebody
Author: John W. Boyd
Publisher:
ISBN:
Category :
Languages : en
Pages : 36
Book Description
Publisher:
ISBN:
Category :
Languages : en
Pages : 36
Book Description
Longitudinal Stability and Control Characteristics at Mach Numbers from 0.70 to 2.22 of Triangular Wing Configuration Equipped with Canard Control, Trailing-edge Flap Control, Or Cambered Forebody [with List of References]
Author:
Publisher:
ISBN:
Category :
Languages : en
Pages : 39
Book Description
Publisher:
ISBN:
Category :
Languages : en
Pages : 39
Book Description
Low-speed Static Longitudinal and Lateral Stability Characteristics of a Variable-incidence Delta-wing Canard Model with High-lift Canard Surfaces
Author: Clarence D. Cone (Jr.)
Publisher:
ISBN:
Category : Airplanes
Languages : en
Pages : 76
Book Description
Publisher:
ISBN:
Category : Airplanes
Languages : en
Pages : 76
Book Description
Effect of Longitudinal and Lateral Controls on Winged Reentry Configuration at Mach 1.97 and Angles of Attack Up to 90°
Author: Gerald V. Foster
Publisher:
ISBN:
Category : Angle of attack (Aerodynamics)
Languages : en
Pages : 20
Book Description
Publisher:
ISBN:
Category : Angle of attack (Aerodynamics)
Languages : en
Pages : 20
Book Description
Static Longitudinal, Directional, and Lateral Stability and Control Data at a Mach Number of 6.83 of the Final Configuration of the X-15 Research Airplane
Author: Jim A. Penland
Publisher:
ISBN:
Category : Aerodynamic measurements
Languages : en
Pages : 150
Book Description
Publisher:
ISBN:
Category : Aerodynamic measurements
Languages : en
Pages : 150
Book Description
Low-speed Static Lateral Stability Characteristics of a Canard Model Having a 60© Triangular Wing and Horizontal Tail
Author: William R. Bates
Publisher:
ISBN:
Category : Airplanes
Languages : en
Pages : 38
Book Description
Publisher:
ISBN:
Category : Airplanes
Languages : en
Pages : 38
Book Description
Span Loadings and Aerodynamic Characteristics for a Series of Tip and Trailing-edge Controls on a 60° Delta Wing at Mach Numbers of 1.61 and 2.01
Author: K. R. Czarnecki
Publisher:
ISBN:
Category : Aerodynamic load
Languages : en
Pages : 124
Book Description
Publisher:
ISBN:
Category : Aerodynamic load
Languages : en
Pages : 124
Book Description
Longitudinal Stability and Control Characteristics at Mach Numbers of 1.41 and 2.01 of a 67 Degree Swept-wing Airplane Configuration with Canard Control Surfaces
Author: M. Leroy Spearman
Publisher:
ISBN:
Category :
Languages : en
Pages : 36
Book Description
Publisher:
ISBN:
Category :
Languages : en
Pages : 36
Book Description