Download or read book Experimental Investigation of the Effect of Vertical tail Size and Length and of Fuselage Shape and Lenghth on the Static Lateral Stability Characteristics Ofa Model with 45 Sweptback Wing and Tail Surfaces written by M.J. Queijo and published by . This book was released on 1951 with total page 29 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Download or read book Experimental Investigation of the Effect of Vertical Tail Size and Length and of Fuselage Shape and Length on the Static Lateral Stability Characteristics of a Model With 45 Deg Sweptback Wing and Tail Surfaces written by and published by . This book was released on 1950 with total page 0 pages. Available in PDF, EPUB and Kindle. Book excerpt: An investigation was made to determine the effects of vertical-tail size and length and of fuselage shape and length on the lateral static stability characteristics of a model with wing and vertical tails having the quarter-chord lines swept back 45 degrees.
Download or read book Experimental Investigation of the Effect of Vertical tail Size and Length and of Fuselage Shape and Length on the Static Lateral Stability Characteristics of a Model with 45 Degree Sweptback Wing and Tail Surfaces written by M. J. Queijo and published by . This book was released on 1950 with total page 59 pages. Available in PDF, EPUB and Kindle. Book excerpt: Results are presented of an investigation made to determine the effects of vertical-tail size and length and of fuselage shape and length on the lateral-static-stability derivatives of a midwing airplane model with 45 degree sweptback wing and tail surfaces. Interference between the various model components also is evaluated.
Download or read book Experimental Investigation of the Effect of Vertical tail Size and Length and of Fuselage Shape and Length on the Static Lateral Stability Characteristics of a Model with 45 Degrees Sweptback Wing and Tail Surfaces written by M.J. Queijo and published by . This book was released on 1951 with total page 29 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Download or read book Experimental Investigation of the Effect of Vertical tail Size and Length and of Fuselage Shape and Length on the Static Lateral Stability Characteristics of a Model with 45 sweptback Wing and Tail Surfaces written by M. J. Queijo and published by . This book was released on 1950 with total page 59 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Download or read book Experimental Determination of the Effect of Horizontal tail Size Tail Length and Vertical Location on Low speed Static Longitudinal Stability and Damping in Pitch of a Model Having 45 sweptback Wing and Tail Surfaces written by Arthur Earl Bryson and published by . This book was released on 1952 with total page 340 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Download or read book Effect of Horizontal tail Size and Tail Length on Low speed Static Longitudinal Stability and Damping in Pitch of a Model Having 45 Sweptback Wing and Tail Surfaces written by Jacob H. Lichtenstein and published by . This book was released on 1951 with total page 40 pages. Available in PDF, EPUB and Kindle. Book excerpt: Wind-tunnel results of the effects of horizontal-tail size and length on the low-speed static longitudinal stability and the steady-state rotary damping in pitch for a complete model with wing and tail surfaces having the quarter-chord lines swept back 45 degrees and aspect ratios of 4 are presented.
Download or read book Investigation of Effect of Sideslip in Lateral Stability Characteristics written by Leo F. Fehlner and published by . This book was released on 1944 with total page 44 pages. Available in PDF, EPUB and Kindle. Book excerpt: Summary: The results of tests of a circular fuselage with various combinations of tail lengths and vertical tail surfaces with and without the horizontal tail surface in the 6- by 6-foot test section of the NACA stability tunnel are reported in the form of diagrams of variation of coefficients of lateral force and yawing moment with angle of yaw and angle of attack. The results of these tests indicated that the change in the unstable yawing moment of the fuselage alone due to increased tail length did not appreciably affect the yawing moment of a fuselage and vertical-tail combination. The addition of a horizontal tail increased the efficiency of the vertical tail in normal-flight attitudes and in the region of negative angles of attack. Existing methods of computing tail effectiveness gave results within ±7 percent of the measured values for the cases computed.
Download or read book Some Effects of Tail Height and Wing Plan Form on the Static Longitudinal Stability Characteristics of a Small scale Model at High Subsonic Speeds written by Albert G. Few and published by . This book was released on 1954 with total page 80 pages. Available in PDF, EPUB and Kindle. Book excerpt: The drag due to lift increases with increasing sweep through the Mach number range. Some increase in bag due to lift is evident decrease in taper ratio for wings having 300of sweep through most of the speed range.
Download or read book Effect of Horizontal tail Location on Low speed Static Longitudinal Stability and Damping in Pitch of a Model Having 45 Sweptback Wing and Tail Surfaces written by Jacob H. Lichtenstein and published by . This book was released on 1951 with total page 34 pages. Available in PDF, EPUB and Kindle. Book excerpt: Wind-tunnel results are presented to show the effect of changes in horizontal-tail location on the low-speed static longitudinal stability and steady-state rotary damping in pitch for a complete model with wing and tail surfaces having the quarter-chord lines swept back 45 degrees.
Download or read book Effects of Wing Position and Horizontal Tail Position on the Static Stability Characteristics of Models With Unswept and 45 Deg Sweptback Surfaces With Some Reference to Mutual Interference written by and published by . This book was released on 1951 with total page 0 pages. Available in PDF, EPUB and Kindle. Book excerpt: An investigation was made to determine the effects of wing position and horizontal tail position on the low speed static longitudinal and static lateral stability characteristics of airplane models having unswept and 45 deg sweptback surfaces. The results indicated that both the unswept and the sweptback low wing low-horizontal-tail configurations were the optimum configurations from the standpoint of longitudinal and lateral stability. The results indicated that, for all wing positions, moving the horizontal tail from the high to the low position resulted in configurations which were longitudinally stable throughout the angle of attack range. For the lateral case, the vertical-tail contribution to the directional stability was increased by moving the wing from the high to the low position because of the favorable sidewash at the vertical tail arising from the wing fuselage interference. The addition of a horizontal tail in the low position produced a further increase in directional stability. The results also indicated that at low angles of attack the effective dihedral due to wing-fuselage interference increased as the wing height was increased - that is, from approximately - 4 deg for the low-wing configuration to 5 deg for the high-wing configuration. This effect could be predicted with fair accuracy by available theory. At low angles of attack, the lateral force on the fuselage was increased because of the end-plate effect when a wing was placed in the high or the low position. However, the lateral force on the fuselage decreased for the low-wing configuration and increased for the high-wing configuration as the angle of attack was increased because of the variation in the distribution of sidewash on the fuselage with angle of attack.
Download or read book Experimental Determination of the Effect of Horizontal tail Size Tail Length and Vertical Location on Low speed Static Longitudinal Stability and Damping in Pitch of a Model Having 45 sweptback Wing and Tail Surfaces written by Jacob H. Lichtenstein and published by . This book was released on 1952 with total page 22 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Download or read book Effect of Vertical Location of a Horizontal Tail on the Static Longitudinal Stability Characteristics of a 45 Degrees Sweptback wing Fuselage Combination of Aspect Ratio 8 at a Reynolds Number of 4 0 X 10 6 written by Reino J. Salmi and published by . This book was released on 1952 with total page 42 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 Investigation of the Influence of Fuselage and Tail Surfaces on Low speed Static Stability and Rolling Characteristics of a Swept wing Model written by John D. Bird and published by . This book was released on 1952 with total page 18 pages. Available in PDF, EPUB and Kindle. Book excerpt: Results are presented of a wind-tunnel investigation to determine influence of the fuselage and tail on static stability and rotary derivatives in roll of a model having 45 degree sweptback win and tail surfaces. The wing alone and the model without the horizontal tail showed marginal longitudinal stability near maximum lift. The longitudinal stability of the complete model was satisfactory. The vertical tail produced larger increments of rate of change of lateral-force and yawing-moment coefficients with wing-tip helix angle than fuselage or the horizontal tail.
Download or read book Effects of Wing and Tail Location on the Aerodynamic Characteristics of an Airplane for Mach Numbers from 0 25 to 4 63 written by and published by . This book was released on 1983 with total page 34 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Download or read book Investigation of the Dynamic Lateral Stability and Control Characteristics of a Model of a Fighter Airplane Without a Horizontal Tail and Equipped with Either Single Or Twin Vertical Tails written by John W. Draper and published by . This book was released on 1949 with total page 24 pages. Available in PDF, EPUB and Kindle. Book excerpt:
