Download or read book Wing flow Measurements of Longitudinal Stability and Control Characteristics of a Canard Airplane Configuration with a 45 Degree Sweptback Wing and a Triangular All movable Control Surface written by Harold L. Crane and published by . This book was released on 1950 with total page 53 pages. Available in PDF, EPUB and Kindle. Book excerpt: Measurements of the longitudinal stability and control characteristics of a canard airplane configuration have been made by the wing-flow method. The distinguishing features of this configuration in addition to the unconventional wing-stabilizer arrangement are the triangular plan form of the all-movable longitudinal control surface, the 45 degree sweptback wing of aspect ratio 4.1, and the slender body of fineness ratio 13.5. The investigation included measurements of lift, pitching moment, and rolling moment of the semispan model, with control settings between -4 degrees and 16 degrees and with the control surface removed. In some cases the angle-of-attack range was as great as from approximately -10 to 30 degrees. Approximate measurements of chord force were made at one stabilizer incidence. The Mach number range covered was from 0.55 to 1.14 at Reynolds numbers of the order of 400,000.
Download or read book Wing flow Measurements of Longitudinal Stability and Control Characteristics of a Canard Airplane Configuration with a 45 Degrees Sweptback Wing and a Triangular Alll movable Control Surface written by Harold L. Crane and published by . This book was released on 1950 with total page 53 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 Low speed Static Lateral Stability Characteristics of a Canard Model Having a 60 Triangular Wing and Horizontal Tail written by William R. Bates and published by . This book was released on 1949 with total page 38 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 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.
Download or read book Scientific and Technical Aerospace Reports written by and published by . This book was released on 1966 with total page 456 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Download or read book Low speed Static Longitudinal and Lateral Stability Characteristics of a Variable incidence Delta wing Canard Model with High lift Canard Surfaces written by Clarence D. Cone (Jr.) and published by . This book was released on 1959 with total page 76 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Download or read book Longitudinal Stability Characteristics at Transonic Speeds of a Canard Configuration Having a 45 Degree Sweptback Wing of Aspect Ratio 6 0 and NACA 65A009 Airfoil Section written by A. James Vitale and published by . This book was released on 1954 with total page 24 pages. Available in PDF, EPUB and Kindle. Book excerpt: A flight investigation has been conducted to determine the longitudinal stability, lift, and drag characteristics at transonic speeds of a rocket-powered model of a canard configuration having a 45 degree swept-back wing of aspect ratio 6.0, taper ratio of 0.6, and NACA 65A009 airfoil section. The canard surface had an aspect ratio of 4.0 and 45 degrees of sweepback. The variations with Mach number of lift, drag, and longitudinal stability for the canard configuration are compared with a tailless and a conventional or tail-last model having the same wing.
Download or read book Index of NASA Technical Publications written by United States. National Aeronautics and Space Administration and published by . This book was released on 1960 with total page 448 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 Applied Mechanics Reviews written by and published by . This book was released on 1962 with total page 1116 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Download or read book A Selected Listing of NASA Scientific and Technical Reports for written by and published by . This book was released on 1960 with total page 450 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Download or read book Wing flow Measurements of Longitudinal Stability and Control Characteristics of a Supersonic Airplane Configuration Having a 42 8 Degree Sweptback Circular Arc Wing with Aspect Ratio 4 0 Taper Ratio 0 50 and Sweptback Tail Surfaces written by Harold L. Crane and published by . This book was released on 1950 with total page 40 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Download or read book The Effects of Mass Distribution on the Low speed Dynamic Lateral Stability and Control Characteristics of a Model with a 45 Sweptback Wing written by Donald E. Hewes and published by . This book was released on 1951 with total page 36 pages. Available in PDF, EPUB and Kindle. Book excerpt: The trends in lateral stability and control produced variations of the mass distribution were determined for a model with a 45 degree sweptback wing. Calculations were made to correlate the trends determined by theory with those determined from tests of a free-flying dynamic model in the Langley free-flight tunnel.
Download or read book Effects of Deflected Wing Tips on the Aerodynamic Characteristics of a Canard Configuration at Mach Numbers from 0 7 to 3 5 written by Victor L. Peterson and published by . This book was released on 1960 with total page 180 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:
