An Experimental Investigation of the Aerodynamic Characteristics of Several Nose-mounted Canard Configurations at Transonic Mach Numbers
Title | An Experimental Investigation of the Aerodynamic Characteristics of Several Nose-mounted Canard Configurations at Transonic Mach Numbers PDF eBook |
Author | James R Burt (Jr.) |
Publisher | |
Pages | 778 |
Release | 1974 |
Genre | Aerodynamics, Transonic |
ISBN |
Experimental aerodynamic investigations were conducted at the CALSPAN Corporation's transonic wind tunnel to determine the aerodynamic characteristics of several nose-mounted canard wing configurations. Canard position, geometry, angular orientation, and model nose shape were varied systematically to determine their effects on model aerodynamics. Angle of attack was varied from -3 to 12 degrees and Mach number was varied from 0.6 to 1.25. Aerodynamic loads were measured separately for each of the four canards and tail surfaces, and the total model.
An Experimental Investigation of the Aerodynamic Characteristics of Nose Mounted Canard Configurations at Supersonic Mach Numbers (1.5 Through 4.5)
Title | An Experimental Investigation of the Aerodynamic Characteristics of Nose Mounted Canard Configurations at Supersonic Mach Numbers (1.5 Through 4.5) PDF eBook |
Author | James R Burt (Jr.) |
Publisher | |
Pages | 352 |
Release | 1976 |
Genre | Aerodynamics, Supersonic |
ISBN |
Experimental aerodynamic investigations were conducted in a supersonic wind tunnel to determine the aerodynamic characteristics of several nose mounted canard wing configurations. Canard position, geometry, angular orientation, and model nose shape were varied systematically to determine their effects on model aerodynamics. The model was tested at angles of attack of -5 to 13 degrees and Mach numbers of 1.5 to 4.5. Aerodynamic loads were measured separately on four canards and tail panels, and the total model. The vapor screen method was used to trace the paths of the vortices shed from the canards. Roll control effectiveness of canards, both with a planar tail and a ring tail was investigated.
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 |
Scientific and Technical Aerospace Reports
Title | Scientific and Technical Aerospace Reports PDF eBook |
Author | |
Publisher | |
Pages | 720 |
Release | 1988 |
Genre | Aeronautics |
ISBN |
Lists citations with abstracts for aerospace related reports obtained from world wide sources and announces documents that have recently been entered into the NASA Scientific and Technical Information Database.
Index of NACA Technical Publications
Title | Index of NACA Technical Publications PDF eBook |
Author | United States. National Advisory Committee for Aeronautics |
Publisher | |
Pages | 388 |
Release | 1959 |
Genre | Aeronautics |
ISBN |
Experimental Investigation of Pressure Distribution and Static Aerodynamic Characteristics for Three Supersonic Impact Ballistic Reentry Shapes at Mach Numbers of 1.93, 2.55, and 3.05
Title | Experimental Investigation of Pressure Distribution and Static Aerodynamic Characteristics for Three Supersonic Impact Ballistic Reentry Shapes at Mach Numbers of 1.93, 2.55, and 3.05 PDF eBook |
Author | |
Publisher | |
Pages | 44 |
Release | 1961 |
Genre | |
ISBN |
Aerodynamic Characteristics at Mach Numbers from 2.30 to 4.50 of a Canard Configuration Having Varied Body Shapes
Title | Aerodynamic Characteristics at Mach Numbers from 2.30 to 4.50 of a Canard Configuration Having Varied Body Shapes PDF eBook |
Author | Donald T. Gregory |
Publisher | |
Pages | 44 |
Release | 1959 |
Genre | |
ISBN |