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Static Stability And Control Of Canard Configurations At Mach Numbers From 070 To 222 Trangular Wing And Canard With Twin Vertical Tails
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Book Synopsis Static Stability and Control of Canard Configurations at Mach Numbers from 0.70 to 2.22 - Trangular Wing and Canard with Twin Vertical Tails by : Victor L. Peterson
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:
Book Synopsis Static Stability and Control of Canard Configurations at Mach Numbers from 0.70 to 2.22 by : Victor L. Peterson
Download or read book Static Stability and Control of Canard Configurations at Mach Numbers from 0.70 to 2.22 written by Victor L. Peterson and published by . This book was released on 1961 with total page 1 pages. Available in PDF, EPUB and Kindle. Book excerpt: The static aerodynamic characteristics of a canard airplane configuration having twin vertical stabilizing surfaces are presented. The model consisted of a wing and canard both of triangular plan form and aspect ratio 2 mounted on a Sears-Haack body of fineness ratio 12.5 and two swept and tapered wing-mounted vertical tails of aspect ratio 1.35. Data are presented for Mach numbers from 0.70 to 2.22 and for angles of attack from -6 degrees to +18 degrees at 0 degrees and 5 degrees sideslip. Tests were made with the canard off and with the canard on. Nominal canard deflection angles ranged from 0 degrees to 10 degrees. The Reynolds number was 3.68 times 10 to the 6th power based on the wing mean aerodynamic chord. Selected portions of the data obtained in this investigation are compared with previously published results for the same model having a single vertical tail instead of twin vertical tails. (Author).
Book Synopsis Static Stability and Control of Canard Configurations at Mach Numbers from 0.70 to 2.22 - Trangular Wing and Canard with Twin Vertical Tails by : Victor L. Peterson
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 38 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis 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 by : Victor L. Peterson
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.
Book Synopsis Static Stability and Control of Canard Configurations at Mach Numbers from 0.70 to 2.22 - Longitudinal Characteristics of an Unswept Wing and Canard by : Victor L. Peterson
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.
Book Synopsis Static Stability and Control of Canard Configurations at Mach Numbers from 0.70 to 2.22 - Triangular Wing and Canard on an Extended Body by : John W. Boyd
Download or read book Static Stability and Control of Canard Configurations at Mach Numbers from 0.70 to 2.22 - Triangular Wing and Canard on an Extended Body written by John W. Boyd and published by . This book was released on 1958 with total page 62 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis 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 by : Victor L. Peterson
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:
Book Synopsis Static Stability and Control of Canard Configurations at Mach Numbers from 0.70 to 2.22 - Longitudinal Characteristics of a Triangular Wing and Canard by : John W. Boyd
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:
Book Synopsis Static Stability and Control Characteristics of a Triangular Wing and Canard Configuration at Mach Numbers from 2.58 to 3.53 by : C. Ernest Hedstrom
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:
Book Synopsis Static Stability and Control of Canard Configurations at Mach Numbers from 0.70 to 2.22 - Lateral-directional Characteristics of an Unswept Wing and Canard by : Victor L. Peterson
Download or read book Static Stability and Control of Canard Configurations at Mach Numbers from 0.70 to 2.22 - Lateral-directional Characteristics of an Unswept Wing and Canard written by Victor L. Peterson and published by . This book was released on 1959 with total page 32 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis The Effects of Wing Vertical Location and Vertical-tail Arrangement on the Stability Characteristics of Canard Airplane Configurations Having Delta and Trapezoidal Planforms at Mach Numbers from 2.38 to 4.00 by : Frank H. Jr Nichols
Download or read book The Effects of Wing Vertical Location and Vertical-tail Arrangement on the Stability Characteristics of Canard Airplane Configurations Having Delta and Trapezoidal Planforms at Mach Numbers from 2.38 to 4.00 written by Frank H. Jr Nichols and published by . This book was released on 1961 with total page 106 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Low-speed Static Stability Characteristics of a Canard Model with a 45 Degree Sweptback Wing and a 60 Degree Triangular Horizontal Control Surface by : John W. Draper
Download or read book Low-speed Static Stability Characteristics of a Canard Model with a 45 Degree Sweptback Wing and a 60 Degree Triangular Horizontal Control Surface written by John W. Draper and published by . This book was released on 1950 with total page 43 pages. Available in PDF, EPUB and Kindle. Book excerpt: An investigation has been made of the low-speed static stability characteristics of a canard model with a 45 degree sweptback wing and a 60 degree triangular horizontal control surface. The model had practically no allowable center-of-gravity range because of longitudinal instability that occurred at moderate and high lift coefficients with horizontal-control-surface incidences of 10 degrees or less. The horizontal control surface produced a sidewash which, at an incidence of 15 degrees at angles of attack greater than 7 degrees, was strong enough to make the model directionally stable with the vertical tail off. This sidewash caused a vertical tail mounted on the fuselage to be destabilizing at angles of attack above 11 degrees. Twin vertical tails mounted at the wing tips did not produce a similar destabilizing effect because they were located outside the sidewash field.
Book Synopsis 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 by : John W. Boyd
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:
Book Synopsis 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] by :
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:
Book Synopsis Effects of Deflected Wing Tips on the Aero- Dynamic Characteristics of a Canard Configuration at Mach Numbers from 0.7 to 3.5 by :
Download or read book Effects of Deflected Wing Tips on the Aero- Dynamic Characteristics of a Canard Configuration at Mach Numbers from 0.7 to 3.5 written by and published by . This book was released on 1960 with total page 94 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Stability and Control Characteristics at a Mach Number of 1.97 of an Airplane Configuration Having Two Types of Variable- Sweep Wings by :
Download or read book Stability and Control Characteristics at a Mach Number of 1.97 of an Airplane Configuration Having Two Types of Variable- Sweep Wings written by and published by . This book was released on 1960 with total page 48 pages. Available in PDF, EPUB and Kindle. Book excerpt:
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