Investigation Of The Aerodynamic Characteristics In Pitch And Sideslip Of A 45c Swept Wing Airplane Configuration With Various Vertical Locations Of The Wing And Horizontal Tail
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| Author | : M. Leroy Spearman |
| Publisher | : |
| Total Pages | : 34 |
| Release | : 1957 |
| Genre | : Airplanes |
| ISBN | : |
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.
| Author | : M. Leroy Spearman |
| Publisher | : |
| Total Pages | : 29 |
| Release | : 1957 |
| Genre | : |
| ISBN | : |
| Author | : M. Leroy Spearman |
| Publisher | : |
| Total Pages | : 36 |
| Release | : 1956 |
| Genre | : Airplanes |
| ISBN | : |
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.
| Author | : M. Leroy Spearman |
| Publisher | : |
| Total Pages | : 36 |
| Release | : 1956 |
| Genre | : Airplanes |
| ISBN | : |
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.
| Author | : M. Leroy Spearman |
| Publisher | : |
| Total Pages | : 39 |
| Release | : 1955 |
| Genre | : Airplanes |
| ISBN | : |
| Author | : M. Leroy Spearman |
| Publisher | : |
| Total Pages | : 159 |
| Release | : 1955 |
| Genre | : |
| ISBN | : |
| Author | : M. Leroy Spearman |
| Publisher | : |
| Total Pages | : 39 |
| Release | : 1955 |
| Genre | : |
| ISBN | : |
| Author | : M. Leroy Spearman |
| Publisher | : |
| Total Pages | : 36 |
| Release | : 1959 |
| Genre | : Airplanes |
| ISBN | : |
| Author | : M. Leroy Spearman |
| Publisher | : |
| Total Pages | : 159 |
| Release | : 1955 |
| Genre | : Airplanes |
| ISBN | : |
| Author | : Odell A. Morris |
| Publisher | : |
| Total Pages | : 32 |
| Release | : 1961 |
| Genre | : Airplanes |
| ISBN | : |
