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
Download 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 full books in PDF, epub, and Kindle. Read online free 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 ebook anywhere anytime directly on your device. Fast Download speed and no annoying ads. We cannot guarantee that every ebooks is available!
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 | : 39 |
Release | : 1955 |
Genre | : |
ISBN | : |
Author | : M. Leroy Spearman |
Publisher | : |
Total Pages | : 39 |
Release | : 1955 |
Genre | : Airplanes |
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 | : United States. National Aeronautics and Space Administration |
Publisher | : |
Total Pages | : 330 |
Release | : 1959 |
Genre | : Aeronautics |
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 | : 159 |
Release | : 1955 |
Genre | : |
ISBN | : |
Author | : |
Publisher | : |
Total Pages | : 494 |
Release | : 1959 |
Genre | : Aeronautics |
ISBN | : |
Author | : United States. National Aeronautics and Space Administration |
Publisher | : |
Total Pages | : 500 |
Release | : 1959 |
Genre | : Aeronautics |
ISBN | : |
Author | : M. Leroy Spearman |
Publisher | : |
Total Pages | : 29 |
Release | : 1957 |
Genre | : |
ISBN | : |