Author: M. Leroy Spearman
Publisher:
ISBN:
Category : Airplanes
Languages : en
Pages : 34
Book Description
An investigation has been conducted in the Langley 4- by 4-foot supersonic pressure tunnel to determine the effects of wing and horizontal-tail vertical location on the aerodynamic characteristics in sideslip at various angles of attack for a supersonic airplane configuration at Mach numbers of 1.41 and 2.01. The basic model was equipped with a wing and horizontal tail, each having 45 degree sweep and an aspect ratio of 4. The wing had a taper ratio of 0.2 and NACA 65A004 sections; the horizontal tail had a taper ratio of 0.4 and NACA 65A006 sections.
Investigation of the Aerodynamic Characteristics in Pitch and Sideslip of a 45© Swept-wing Airplane Configuration with Various Vertical Locations of the Wing and Horizontal Tail
Author: M. Leroy Spearman
Publisher:
ISBN:
Category : Airplanes
Languages : en
Pages : 34
Book Description
An investigation has been conducted in the Langley 4- by 4-foot supersonic pressure tunnel to determine the effects of wing and horizontal-tail vertical location on the aerodynamic characteristics in sideslip at various angles of attack for a supersonic airplane configuration at Mach numbers of 1.41 and 2.01. The basic model was equipped with a wing and horizontal tail, each having 45 degree sweep and an aspect ratio of 4. The wing had a taper ratio of 0.2 and NACA 65A004 sections; the horizontal tail had a taper ratio of 0.4 and NACA 65A006 sections.
Publisher:
ISBN:
Category : Airplanes
Languages : en
Pages : 34
Book Description
An investigation has been conducted in the Langley 4- by 4-foot supersonic pressure tunnel to determine the effects of wing and horizontal-tail vertical location on the aerodynamic characteristics in sideslip at various angles of attack for a supersonic airplane configuration at Mach numbers of 1.41 and 2.01. The basic model was equipped with a wing and horizontal tail, each having 45 degree sweep and an aspect ratio of 4. The wing had a taper ratio of 0.2 and NACA 65A004 sections; the horizontal tail had a taper ratio of 0.4 and NACA 65A006 sections.
Investigation of the Aerodynamic Characteristics in Pitch and Sideslip of a 45 Degree Swept-wing Airplane Configuration with Various Vertical Locations of the Wing and Horizontal Tail
Investigation of Aerodynamic Characteristics in Pitch and Sideslip of a 45 Degree Sweptback-wing Airplane Model with Various Vertical Locations of Wing and Horizontal Tail
Author: M. Leroy Spearman
Publisher:
ISBN:
Category : Airplanes
Languages : en
Pages : 36
Book Description
An investigation has been conducted in the Langley 4- by 4-foot supersonic pressure tunnel to determine the effects of various vertical locations of the wing and horizontal tail on the aerodynamic characteristics in pitch of a supersonic airplane configuration at a Mach number of 2.01. The model is equipped with a wing and horizontal tail, each having a 45 degree sweep and an aspect ratio of 4. The wing had a taper ratio of 0.2 with NACA 65A004 airfoil sections, whereas the horizontal tail had a taper ratio of 0.6 with NACA 65A006 airfoil sections.
Publisher:
ISBN:
Category : Airplanes
Languages : en
Pages : 36
Book Description
An investigation has been conducted in the Langley 4- by 4-foot supersonic pressure tunnel to determine the effects of various vertical locations of the wing and horizontal tail on the aerodynamic characteristics in pitch of a supersonic airplane configuration at a Mach number of 2.01. The model is equipped with a wing and horizontal tail, each having a 45 degree sweep and an aspect ratio of 4. The wing had a taper ratio of 0.2 with NACA 65A004 airfoil sections, whereas the horizontal tail had a taper ratio of 0.6 with NACA 65A006 airfoil sections.
Investigation of Aerodynamic Characteristics in Pitch and Sideslip of a 45 Degree Sweptback-wing Airplane Model with Various Vertical Locations of Wing and Horizontal Tail
Author: M. Leroy Spearman
Publisher:
ISBN:
Category : Airplanes
Languages : en
Pages : 36
Book Description
An investigation has been conducted in the Langley 4- by 4-foot supersonic pressure tunnel to determine the effects of various vertical locations of the wing and horizontal tail on the aerodynamic characteristics in pitch of a supersonic airplane configuration at a Mach number of 2.01. The model is equipped with a wing and horizontal tail, each having a 45 degree sweep and an aspect ratio of 4. The wing had a taper ratio of 0.2 with NACA 65A004 airfoil sections, whereas the horizontal tail had a taper ratio of 0.6 with NACA 65A006 airfoil sections.
Publisher:
ISBN:
Category : Airplanes
Languages : en
Pages : 36
Book Description
An investigation has been conducted in the Langley 4- by 4-foot supersonic pressure tunnel to determine the effects of various vertical locations of the wing and horizontal tail on the aerodynamic characteristics in pitch of a supersonic airplane configuration at a Mach number of 2.01. The model is equipped with a wing and horizontal tail, each having a 45 degree sweep and an aspect ratio of 4. The wing had a taper ratio of 0.2 with NACA 65A004 airfoil sections, whereas the horizontal tail had a taper ratio of 0.6 with NACA 65A006 airfoil sections.
Investigation of the Aerodynamic Characteristics in Pitch and Sideslip of a 45° Sweptback-wing Airplane Model with Various Vertical Locations of the Wing and Horizontal Tail
Author: M. Leroy Spearman
Publisher:
ISBN:
Category : Airplanes
Languages : en
Pages : 39
Book Description
Publisher:
ISBN:
Category : Airplanes
Languages : en
Pages : 39
Book Description
Investigation of Aerodynamic Characteristics in Pitch and Sideslip of a 45 Degree Sweptback-wing Airplane Model with Various Vertical Locations of Wing and Horizontal Tail
Investigation of the Aerodynamic Characteristics in Pitch and Sideslip of a 45 Degree Sweptback-wing Airplane Model with Various Vertical Locations of the Wing and Horizontal Tail - Effect of Wing Location and Geometric Dihedral for the Wing-body Combination, M
Investigation of Aerodynamic Characteristics in Pitch and Sideslipets of a 45° Sweptback-wing Airplane Model with Various Vertical Locations of Wing and Horizontal Tail
Author: M. Leroy Spearman
Publisher:
ISBN:
Category : Airplanes
Languages : en
Pages : 36
Book Description
Publisher:
ISBN:
Category : Airplanes
Languages : en
Pages : 36
Book Description
Investigation of Aerodynamic Characteristics in Pitch and Sideslipets of a 45° Sweptback-wing Airplane Model with Various Vertical Locations of Wing and Horizontal Tail
Author: M. Leroy Spearman
Publisher:
ISBN:
Category : Airplanes
Languages : en
Pages : 159
Book Description
Publisher:
ISBN:
Category : Airplanes
Languages : en
Pages : 159
Book Description
Static Longitudinal and Lateral Aerodynamic Characteristics at a Mach Number of 2.20 of a V/STOL Airplane Configuration with a Variable-sweep Wing and with a Skewed Wing Design
Author: Odell A. Morris
Publisher:
ISBN:
Category : Airplanes
Languages : en
Pages : 32
Book Description
Publisher:
ISBN:
Category : Airplanes
Languages : en
Pages : 32
Book Description