Download or read book Investigation of the Effect of Balancing Tabs on the Hinge moment Characteristics of a Trailing edge Flap type Control on a Trapezoidal Wing at a Mach Number of 1 61 written by Douglas R. Lord and published by . This book was released on 1954 with total page 23 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Download or read book Hinge moment and Effectiveness Characteristics of an Aspect ratio 8 2 Flap type Control on a 60 Delta Wing at Mach Numbers from 0 72 to 1 96 written by Lawrence Duncan Guy and published by . This book was released on 1957 with total page 54 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Download or read book Control Hinge moment and Effectiveness Characteristics of Several Interchangeable Tip Controls on a 60 Degree Delta Wing at Mach Numbers of 1 41 1 62 and 1 96 written by Odell A. Morris and published by . This book was released on 1953 with total page 33 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Download or read book Hinge moment and Effectiveness Characteristics of an Aspect ratio 8 2 Flap type Control on a 60 Degrees Delta Wing at Mach Numbers from 0 72 to 1 96 written by Lawrence D. Guy and published by . This book was released on 1957 with total page 53 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Download or read book Hinge Moment and Effectiveness of an Unswept Constant chord Control and an Overhang balanced Swept Hinge line Control on an 80 Degree Swept Pointed Wing at Mach Numbers from 0 75 to 1 96 written by Lawrence D. Guy and published by . This book was released on 1956 with total page 39 pages. Available in PDF, EPUB and Kindle. Book excerpt: An investigation of a semi-span wing-fuselage model having an 80 degree swept pointed wing with either an unbalanced constant-chord control or an overhang-balanced swept hinge-line control was conducted in the Langley 9- by 12-inch blowdown tunnel. Control hinge moments and effectiveness characteristics were obtained over an angle-of-attack range of plus or minus 16 degrees at control deflections up to 25 degrees. Data were obtained at Mach numbers from 0.75 to 1.96.
Download or read book Analysis of Available Data on the Effects of Tabs on Control surface Hinge Moments written by Stewart M. Crandall and published by . This book was released on 1946 with total page 28 pages. Available in PDF, EPUB and Kindle. Book excerpt: An analysis was made of the hinge-moment effectiveness of tabs based on the available two- and three-dimensional tab data. The results of the analysis indicated that the effects of tabs on control-surface hinge moments can be estimated from geometric characteristics of the tab-flap-airfoil combination with a reasonable degree of accuracy.
Download or read book Rocket powered model Investigation of the Hinge moment and Normal force Characteristics of a Half diamond Tip Control on a 60 Degree Sweptback Diamond Wind Between Mach Numbers of 0 5 and 1 3 written by James D. Church and published by . This book was released on 1954 with total page 30 pages. Available in PDF, EPUB and Kindle. Book excerpt: A free-flight investigation has been conducted to determine normal-force and hinge-moment characteristics of a half-diamond tip control on a diamond wing having 60 degree sweptback leading edges and 30 degree sweptforward trailing edges through a range of Mach number of 0.5 to 1.3. Results indicate that the control could be so hinged that very small hinge-moments due to control deflection would be obtained at low angles of attack over the speed range tested, although nonlinear variations of hinge moment with angle of attack were present in the transonic range.
Download or read book Experimental Hinge Moments on Freely Oscillating Flap type Control Surfaces written by C. William Martz and published by . This book was released on 1956 with total page 29 pages. Available in PDF, EPUB and Kindle. Book excerpt: Oscillatory hinge-moment characteristics have been obtained from free-flight tests of two rocket-powered models each equipped with a 60 degree sweptback clipped delta wing featuring an unbalanced, constant-chord, full-span trailing-edge control. One control had a sharp trailing edge, and the other had a trailing-edge thickness equal to 1/2 the thickness at the hinge line. Data were obtained at zero angle of attack and control reduced frequencies ranged from 0.09 to 0.035. The Mach number range of the investigation was from 0.4 to 1.9.
Download or read book Recent Information on Flap and Tip Controls written by Douglas R. Lord and published by . This book was released on 1953 with total page 26 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Download or read book Hinge moment Characteristics for a Series of Controls and Balancing Devices on a 60 Degrees Delta Wing at Mach Numbers of 1 61 and 2 01 written by Douglas R. Lord and published by . This book was released on 1957 with total page 68 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Download or read book Control surface Hinge moment and Elevon Normal force Characteristics at Transonic Speeds on a Manned Lifting Entry Vehicle written by and published by . This book was released on 1966 with total page 28 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Download or read book Investigation of Transonic Speeds of the Effect of a Positive lift Balancing Tab on the Hinge moment and Lift Characteristics of a Full span Flap on a Tapered 45 Degree Sweptback Wing of Aspect Ratio 3 written by Vernard E. Lockwood 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 Control Hinge moment and Effectiveness Characteristics of a Horn balanced Flap type Control on a 55 Degree Sweptback Triangular Wing of Aspect Ratio 3 5 at Mach Numbers of 1 41 1 62 and 1 96 written by Lawrence D. Guy and published by . This book was released on 1953 with total page 29 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Download or read book Experimental Hinge Moments on Two Freely Oscillating Trailing edge Controls Hinged at 55 Percent Control Chord written by C. William Martz and published by . This book was released on 1957 with total page 28 pages. Available in PDF, EPUB and Kindle. Book excerpt: Oscillatory hinge-moment characteristics have been obtained from free-flight tests of two rocket-powered models having a 60 degrees delta wing with a constant-chord, full-span, trailing-edge control with blunted trailing-edge, and hinge line at 55 percent control chord. One control had a row of chordwise slots near its leading edge. Data were obtained at near zero angle of attack and variable deflection amplitudes up to plus or minus 5 degrees. Control reduced frequencies ranged from 0.12 to 0.04,and Mach numbers ranged from 0.50 to 1.8.
Download or read book Hinge moment Lift and Pitching moment Characteristics of a Flap type Control Surface Having Various Hinge line Locations on a 4 Percent thick 80 Degree Delta Wing written by Robert F. Thompson and published by . This book was released on 1954 with total page 73 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Download or read book The Effect of a Change in Airfoil Section on the Hinge moment Characteristics of a Half delta Tip Control with a 60 Degree Sweep Angle at a Mach Number of 6 9 written by David E. Fetterman and published by . This book was released on 1954 with total page 14 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Download or read book Analysis of Hinge Moment Data for Rectangular and Near Trailing Edge Controls at Supersonic and Transonic Speeds written by D. Isaacs and published by . This book was released on 1965 with total page 61 pages. Available in PDF, EPUB and Kindle. Book excerpt:
