Download or read book Static Stability Characteristics of a Delta Winged Airplane Configuration with Nacelles a Trapezoidal Canard and a Drooped Tail at Mach Numbers from 0 70 to 3 52 written by and published by . This book was released on 1963 with total page 68 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Download or read book Static Stability Characteristics of a Delta winged Configuration with a Canard Control and Nacelles at Mach Numbers from 0 25 to 3 50 written by LeRoy S. Fletcher and published by . This book was released on 1962 with total page 108 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 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 Low speed Static Stability Characteristics of a Cambered delta wing Model written by John M. Riebe and published by . This book was released on 1956 with total page 32 pages. Available in PDF, EPUB and Kindle. Book excerpt: An investigation was made in the Langley 300 MPH 7- by 10-foot tunnel to determine the static stability characteristics of a cambered-delta-wing model. The cambered delta wing was derived from a segment of a cone selected so that the projected plan form with a wing dihedral angle of zero degrees was the same as a 60 degree delta wing. The projected plan form had an aspect ratio of 2.31.
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 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).
Download or read book Static Longitudinal and Lateral Aerodynamic Characteristics at a Mach Number of 2 01 of a Tailless Delta V STOL Configuration Having Variable sweep Wing Panels written by M. Leroy Spearman and published by . This book was released on 1961 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 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 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 Effect at High Subsonic Speeds of Fuselage Forebody Strakes on the Static Stability and Vertical tail load Characteristics of a Complete Model Having a Delta Wing written by Edward Charles Polhamus and published by . This book was released on 1961 with total page 36 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 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 Delta Wing written by Cornelius Driver and published by . This book was released on 1960 with total page 30 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Download or read book Effects of Wing Position and Fuselage Size on the Low speed Static and Rolling Stability Characteristics of a Delta wing Model written by Alex Goodman and published by . This book was released on 1954 with total page 82 pages. Available in PDF, EPUB and Kindle. Book excerpt: An investigation was made to determine the effects of wing position and fuselage size on the low-speed static and rolling stability characterististics of airplane models having a triangular wing and vertical tail surfaces.
Download or read book Rocket model Investigation of Longitudinal Stability and Drag Characteristics of an Airplane Configuration Have a 60 Delta Wing and a High Unwept Horizontal Tail written by Robert F. Peck and published by . This book was released on 1953 with total page 32 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 Effects of Wing Incidence on the Longitudinal Trim Characteristics of a Cambered 70 Delta wing Configuration at Mach Numbers 3 0 to 5 0 written by Warren F. Ahtye and published by . This book was released on 1960 with total page 56 pages. Available in PDF, EPUB and Kindle. Book excerpt:
