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
Download and Read 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 full books in PDF, ePUB, and Kindle. Read online free 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 ebook anywhere anytime directly on your device. We cannot guarantee that every ebooks is available!
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 | : |
| Total Pages | : 34 |
| Release | : 1957 |
| Genre | : Airplanes |
| ISBN | : |
Download 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 Book in PDF, Epub and Kindle
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 Related Books
Pages: 34
Pages: 29
Pages: 36
Pages: 36
Pages: 39
