Download or read book Longitudinal Stability and Control Characteristics at Mach Numbers from 0 70 to 2 22 of a Triangular Wing Configuration Equipped with a Canard Control a Trailing edge flap Control Or a Cambered Forebody written by John W. Boyd and published by . This book was released on 1959 with total page 36 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Download or read book Longitudinal Stability and Control Characteristics at Mach Numbers from 0 70 to 2 22 of Triangular Wing Configuration Equipped with Canard Control Trailing edge Flap Control Or Cambered Forebody with List of References written by and published by . This book was released on 1959 with total page 39 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Download or read book Index to NASA Technical Publications written by United States. National Aeronautics and Space Administration and published by . This book was released on 1960-07 with total page pages. Available in PDF, EPUB and Kindle. Book excerpt:

Download or read book Longitudinal and Lateral Stability and Control Characteristics at Mach Number 2 01 of a 60 Degree Delta wing Airplane Configuration Equipped with a Canard Control and with Wing Trailing edge Flap Controls written by M. Leroy Spearman and published by . This book was released on 1958 with total page 51 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Download or read book Effects of Wing Height on the Stability and Control Characteristics at a Mach Number of 2 01 of a Canard Airplane Configuration with a 70 Deg Delta Wing written by and published by . This book was released on 1960 with total page 36 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Download or read book Static Stability and Control of Canard Configurations at Mach Numbers from 0 70 to 2 22 Trangular Wing and Canard with Twin Vertical Tails written by Victor L. Peterson and published by . This book was released on 1961 with total page 44 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Download or read book Longitudinal Stability and Control Characteristics at Mach Numbers of 1 41 and 2 01 of a 67 Degree Swept wing Airplane Configuration with Canard Control Surfaces written by M. Leroy Spearman and published by . This book was released on 1958 with total page 36 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Download or read book Static Stability and Control Characteristics of a Triangular Wing and Canard Configuration at Mach Numbers from 2 58 to 3 53 written by C. Ernest Hedstrom and published by . This book was released on 1958 with total page 62 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Download or read book Static Stability and Control of Canard Configurations at Mach Numbers from 0 70 to 2 22 Longitudinal Characteristics of a Triangular Wing and Canard written by John W. Boyd and published by . This book was released on 1958 with total page 32 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Download or read book 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 written by Victor L. Peterson and published by . This book was released on 1958 with total page 31 pages. Available in PDF, EPUB and Kindle. Book excerpt: 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.

Download or read book Static Longitudinal Aerodynamic Characteristics of Close coupled Wing canard Configurations at Mach Numbers from 1 60 to 2 86 written by Samuel M. Dollyhigh and published by . This book was released on 1971 with total page 126 pages. Available in PDF, EPUB and Kindle. Book excerpt: An experimental investigation was made in the Mach number range from 1.60 to 2.86 to determine the static longitudinal aerodynamic characteristics of close-coupled wing-canard configurations. Three canards, ranging in exposed planform area from 17.5 to 30.0 percent of the wing reference area, were employed in this investigation. The canards were either located in the plane of the wing or in a position 18.5 percent of the wing mean geometric chord above the wing plane. Most data obtained were for a model with a 60 deg leading-edge-sweep wing; however, a small amount of data were obtained for a 44 deg leading-edge-sweep wing. The model utilized two balances to isolate interference effects between wing and canard. In general, it was determined that at angle of attack for all configurations investigated with the canard in the plane of the wing an unfavorable interference exists which causes the additional lift on the canard generated by a canard deflection to be lost on the wing due to an increased downwash at the wing from the canard. Further, this interference decreased somewhat with increasing Mach number. Raising the canard above the plane of the wing also greatly decreased the interference of the canard deflection on the wing lift. However, at Mach 2.86 the presence of the canard in the high position had a greater unfavorable interference effect at high angles of attack than the canard in the wing plane. This interference resulted in the in-plane canard having better trimmed performance at Mach 2.86 for the same center-of-gravity location.

Download or read book The Static Longitudinal Characteristics at Mach Numbers Up to 0 95 of a Triangular wing Canard Model Having a Triangular Control written by Jack D. Stephenson and published by . This book was released on 1951 with total page 72 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Download or read book Static Stability and Control of Canard Configurations at Mach Numbers from 0 7 to 2 22 Lateral directional Characteristics of a Triangular Wing and Canard written by Victor L. Peterson and published by . This book was released on 1958 with total page 76 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Download or read book Span Loadings and Aerodynamic Characteristics for a Series of Tip and Trailing edge Controls on a 60 Delta Wing at Mach Numbers of 1 61 and 2 01 written by K. R. Czarnecki and published by . This book was released on 1959 with total page 124 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Download or read book Longitudinal and Lateral Stability and Control Characteristics of Various Combinations of Component Parts of 2 Canard Airplane Configurations at Mach Numbers of 1 41 and 2 01 with List of References written by and published by . This book was released on 1958 with total page 104 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Download or read book Static Stability and Control of Canard Configurations at Mach Numbers from 0 70 to 2 22 Longitudinal Characteristics of an Unswept Wing and Canard written by Victor L. Peterson and published by . This book was released on 1958 with total page 29 pages. Available in PDF, EPUB and Kindle. Book excerpt: 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 3.1 unswept wing, an aspect ratio 3.0 unswept canard, a low aspect ratio vertical tail, and a Sears-Haack body. The hinge line of the canard was in the extended chord plane of the wing, 1.33 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.

Download or read book Effects of Forebody Length on the Stability and Control Characteristics at a Mach Number of 2 01 of a Canard Airplane Configuration with a Trapezoidal Aspect ratio 3 Wing written by M. Leroy Spearman and published by . This book was released on 1962 with total page 36 pages. Available in PDF, EPUB and Kindle. Book excerpt: