Aerodynamic Characteristics of a Canard and an Outboard-tail Airplane Model at High Subsonic Speeds
Title | Aerodynamic Characteristics of a Canard and an Outboard-tail Airplane Model at High Subsonic Speeds PDF eBook |
Author | Paul G. Fournier |
Publisher | |
Pages | 72 |
Release | 1961 |
Genre | Aerodynamic load |
ISBN |
Aerodynamic Characteristics of a Canard and an Outboard-tail Airplane Model at High Subsonic Speeds
Title | Aerodynamic Characteristics of a Canard and an Outboard-tail Airplane Model at High Subsonic Speeds PDF eBook |
Author | Paul G. Fournier |
Publisher | |
Pages | 1 |
Release | 1961 |
Genre | |
ISBN |
An investigation was made in the Langley highspeed 7- by 10-foot tunnel through a range of Mach numbers from 0.60 to 0.95 of the static longitudinal and lateral stability and control characteristics of a canard airplane configuration and an outboard-tail configuration. The canard model had a twisted wing with approximately 67 degrees o sweepback and an aspect ratio of 2.91 and was tested with three trapezoidal canard surfaces having ratios of exposed area to wing area of 0.032, 0.076, and 0.121. The canard model had a single body-mounted vertical tail. The outboard-tail model had its horizontal- and vertical-tail surfaces mounted on slender bodies attached to the wing tips and located to the rear and outboard of the 67 degrees sweptback wing of aspect ratio 1.00. The data, which are presented with limited analysis, provide information at high subsonic speeds on these two types of high-speed airplanes which have previously been tested at supersonic speeds and reported in NACA RM L58B07 and NACA RM L58E20 (AD-153 929 and AD-221 852). (Author).
Aerodynamic Characteristics of a Canard and an Outboard-tail Airplane Model at a Mach Number of 2.01
Title | Aerodynamic Characteristics of a Canard and an Outboard-tail Airplane Model at a Mach Number of 2.01 PDF eBook |
Author | M. Leroy Spearman |
Publisher | |
Pages | 35 |
Release | 1958 |
Genre | |
ISBN |
Effect of Vertical-tail Location on the Aerodynamic Characteristics at Subsonic Speeds of a Close-coupled Canard Configuration
Title | Effect of Vertical-tail Location on the Aerodynamic Characteristics at Subsonic Speeds of a Close-coupled Canard Configuration PDF eBook |
Author | Jarrett K. Huffman |
Publisher | |
Pages | 56 |
Release | 1975 |
Genre | Airplanes |
ISBN |
NASA Technical Note
Title | NASA Technical Note PDF eBook |
Author | |
Publisher | |
Pages | 842 |
Release | 1963 |
Genre | |
ISBN |
Static Longitudinal Aerodynamic Characteristics of an Elastic Canard-fuselage Configuration as Measured in Air and in Freon-12 at Mach Numbers Up to 0.92
Title | Static Longitudinal Aerodynamic Characteristics of an Elastic Canard-fuselage Configuration as Measured in Air and in Freon-12 at Mach Numbers Up to 0.92 PDF eBook |
Author | Edward Carson Yates |
Publisher | |
Pages | 192 |
Release | 1963 |
Genre | Airplanes |
ISBN |
Longitudinal Aerodynamic Characteristics of a 1/30-scale Subsonic Canard-airplane Model Having a Wing with an Aspect Ratio of 3.6 at Mach Numbers from 0.30 to 0.98
Title | Longitudinal Aerodynamic Characteristics of a 1/30-scale Subsonic Canard-airplane Model Having a Wing with an Aspect Ratio of 3.6 at Mach Numbers from 0.30 to 0.98 PDF eBook |
Author | |
Publisher | |
Pages | 168 |
Release | 1962 |
Genre | |
ISBN |