An Investigation at Mach Numbers from 0.20 to 4.63 of the Aerodynamic Performance, Static Stability, and Trimming Characteristics of a Canard Configuration Designed for Efficient Supersonic Cruise Flight
| Title | An Investigation at Mach Numbers from 0.20 to 4.63 of the Aerodynamic Performance, Static Stability, and Trimming Characteristics of a Canard Configuration Designed for Efficient Supersonic Cruise Flight PDF eBook |
| Author | |
| Publisher | |
| Pages | 88 |
| Release | 1961 |
| Genre | |
| ISBN |
Download An Investigation at Mach Numbers from 0.20 to 4.63 of the Aerodynamic Performance, Static Stability, and Trimming Characteristics of a Canard Configuration Designed for Efficient Supersonic Cruise Flight Book in PDF, Epub and Kindle
Aerodynamic Characteristics at Mach Numbers from 0.20 to 4.63 of a Canard-type Supersonic Commercial Air Transport Configuration
| Title | Aerodynamic Characteristics at Mach Numbers from 0.20 to 4.63 of a Canard-type Supersonic Commercial Air Transport Configuration PDF eBook |
| Author | |
| Publisher | |
| Pages | 124 |
| Release | 1962 |
| Genre | |
| ISBN |
Download Aerodynamic Characteristics at Mach Numbers from 0.20 to 4.63 of a Canard-type Supersonic Commercial Air Transport Configuration Book in PDF, Epub and Kindle
Static Stability and Control of Canard Configurations at Mach Numbers from 0.70 to 2.22 - Trangular Wing and Canard with Twin Vertical Tails
| Title | Static Stability and Control of Canard Configurations at Mach Numbers from 0.70 to 2.22 - Trangular Wing and Canard with Twin Vertical Tails PDF eBook |
| Author | Victor L. Peterson |
| Publisher | |
| Pages | 44 |
| Release | 1961 |
| Genre | Aerodynamics |
| ISBN |
Download Static Stability and Control of Canard Configurations at Mach Numbers from 0.70 to 2.22 - Trangular Wing and Canard with Twin Vertical Tails Book in PDF, Epub and Kindle
Aerodynamic Characteristics at Mach Numbers from 0.60 to 1.16 of a Canard Configuration Designed for Supersonic Cruise Flight
| Title | Aerodynamic Characteristics at Mach Numbers from 0.60 to 1.16 of a Canard Configuration Designed for Supersonic Cruise Flight PDF eBook |
| Author | |
| Publisher | |
| Pages | 38 |
| Release | 1960 |
| Genre | |
| ISBN |
Download Aerodynamic Characteristics at Mach Numbers from 0.60 to 1.16 of a Canard Configuration Designed for Supersonic Cruise Flight Book in PDF, Epub and Kindle
Static Aerodynamic Characteristics at Mach Numbers from 2.50 to 4.63 of a Staged Airplane Model Designed for Cruise Above Mach 5
| Title | Static Aerodynamic Characteristics at Mach Numbers from 2.50 to 4.63 of a Staged Airplane Model Designed for Cruise Above Mach 5 PDF eBook |
| Author | |
| Publisher | |
| Pages | 62 |
| Release | 1964 |
| Genre | |
| ISBN |
Download Static Aerodynamic Characteristics at Mach Numbers from 2.50 to 4.63 of a Staged Airplane Model Designed for Cruise Above Mach 5 Book in PDF, Epub and Kindle
Aerodynamic Characteristics at Mach Numbers of 1.5, 1.8, and 2.0 of a Blended Wing-body Configuration with and Without Integral Canards
| Title | Aerodynamic Characteristics at Mach Numbers of 1.5, 1.8, and 2.0 of a Blended Wing-body Configuration with and Without Integral Canards PDF eBook |
| Author | A. Warner Robins |
| Publisher | |
| Pages | 68 |
| Release | 1979 |
| Genre | Hypersonic planes |
| ISBN |
Download Aerodynamic Characteristics at Mach Numbers of 1.5, 1.8, and 2.0 of a Blended Wing-body Configuration with and Without Integral Canards Book in PDF, Epub and Kindle
Static Stability and Control of Canard Configurations at Mach Numbers from 0.70 to 2.22 - Longitudinal Characteristics of a Triangular Wing and Unswept Canard
| Title | Static Stability and Control of Canard Configurations at Mach Numbers from 0.70 to 2.22 - Longitudinal Characteristics of a Triangular Wing and Unswept Canard PDF eBook |
| Author | Victor L. Peterson |
| Publisher | |
| Pages | 31 |
| Release | 1958 |
| Genre | Airplanes |
| ISBN |
Download Static Stability and Control of Canard Configurations at Mach Numbers from 0.70 to 2.22 - Longitudinal Characteristics of a Triangular Wing and Unswept Canard Book in PDF, Epub and Kindle
The results of an investigation of the static longitudinal stability and control characteristics of a canard airplane configuration are presented without analysis for the Mach number range from 0.70 to 2.22. The configuration consisted of an aspect ratio vertical tail, and a Sears-Haack body. The hinge line of the canard was in the extended chord plane of the wing, 1.15 wing mean aerodynamic chords ahead of the reference center of moments. The ratio of the area of the exposed canard panels to the total area of the wing is 8.1 percent. Data are presented for various combinations of the canard, wing, and vertical tail for an angle-of-attack range from -6 to 18 degrees. The canard deflection angles ranged from 0 to 20 degrees.