The Effect Of A Change In Airfoil Section On The Hinge Moment Characteristics Of A Half Delta Tip Control With A 60c Sweep Angle At A Mach Number Of 69

Author : David E. Fetterman
Publisher :
ISBN 13 :
Total Pages : 18 pages
Book Rating : 4.74/5 ( download)

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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© 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 18 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Author : Odell A. Morris
Publisher :
ISBN 13 :
Total Pages : 38 pages
Book Rating : 4.26/5 ( download)

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Download or read book Control Hinge-movement and Effectiveness Characteristics of Several Interchangeable Tip Controls on a 60© 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 38 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Author : Lawrence Duncan Guy
Publisher :
ISBN 13 :
Total Pages : 42 pages
Book Rating : 4.98/5 ( download)

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Download or read book Effects of an Inset Tab on the Hinge-moment and Effectiveness Characteristics of an Unswept Trailing-edge Control on a 60© Delta Wing at Mach Numbers from 0.75 to 1.96 written by Lawrence Duncan Guy and published by . This book was released on 1955 with total page 42 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Author : Lawrence D. Guy
Publisher :
ISBN 13 :
Total Pages : 52 pages
Book Rating : 4.17/5 ( download)

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Download or read book Effects of Overhang Balance on the Hinge-moment and Effectiveness Characteristics of an Unswept Trailing-edge Control on a 60 Degree Delta Wing at Transonic and Supersonic Speeds written by Lawrence D. Guy and published by . This book was released on 1954 with total page 52 pages. Available in PDF, EPUB and Kindle. Book excerpt: A wind-tunnel investigation has been made of two unswept, partial-span, flap-type controls (differing only in hinge-line location) mounted on a 60 degree delta wing. One control was unbalanced and the other has a 100-percent overhang balance. Control hinge moments as well as aerodynamic characteristics of the complete wing-body combination were obtained for control deflections from 0 to 40 degrees over an angle-of-attack range of plus or minus 12 degrees at Mach numbers from 0.75 to 1.96. Reynolds numbers varied between 2,200,000 and 2,200,000. Expressions derived from linear theory for the hinge-moment coefficient due to angle of attack for unswept partial-span controls (which extend neither to the wing tip nor to the wing center line) on triangular wings having subsonic leading edges are given in an appendix.

Author : Paul E. Purser
Publisher :
ISBN 13 :
Total Pages : 34 pages
Book Rating : 4.61/5 ( download)

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Download or read book Collection and Analysis of Hinge-moment Data on Control-surface Tabs written by Paul E. Purser and published by . This book was released on 1947 with total page 34 pages. Available in PDF, EPUB and Kindle. Book excerpt: Various wind-tunnel data on the hinge-moment characteristics of control-surface tabs have been collected and analyzed. The data, all of which are for plain unbalanced tabs, were obtained from force tests of models in two- and three-dimensional flow and from pressure-distribution measurements on models in two-dimensional flow. Some data that show the effects of Mach number on tab hinge moments for representative conventional and NACA 6-series airfoil sections are presented.

Author : William C. Sleeman
Publisher :
ISBN 13 :
Total Pages : 34 pages
Book Rating : 4.03/5 ( download)

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Download or read book Aerodynamic Characteristics of a Delta Wing with Leading Edge Swept Back 45 Degrees, Aspect Ratio 4, and NACA 65A006 Airfoil Section written by William C. Sleeman and published by . This book was released on 1949 with total page 34 pages. Available in PDF, EPUB and Kindle. Book excerpt: This paper presents the results of the investigation of wing-alone and wing-fuselage combination employing a delta wing having 45 degree sweepback of the leading edge, aspect ratio 4, and an NACA 65A006 airfoil section. Lift, drag, pitching moment, and root bending moment were obtained for these configurations. In addition, effective downwash angles and dynamic-pressure characteristics in the region of a probable tail location also were obtained for these configurations, and are presented for a range of tail heights at one tail length. In order to expedite publishing of these data, only a brief analysis is included.

Author : William E. Palmer
Publisher :
ISBN 13 :
Total Pages : 36 pages
Book Rating : 4.66/5 ( download)

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Download or read book A Transonic Wind-tunnel Investigation of the Longitudinal Force and Moment Characteristics of Two Delta Wings and One Clipped-tip Delta Wing of 4 Percent Thickness on a Slender Body written by William E. Palmer and published by . This book was released on 1955 with total page 36 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Author : J. D. Bird
Publisher :
ISBN 13 :
Total Pages : 74 pages
Book Rating : 4.94/5 ( download)

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Download or read book A Effect of Leakage Past Aileron Nose on Aerodynamic Characteristics of Plain and Internally Balanced Ailerons on NACA 66(215)-216 written by J. D. Bird and published by . This book was released on 1945 with total page 74 pages. Available in PDF, EPUB and Kindle. Book excerpt: Summary: An investigation has been made in two-dimensional flow to determine the effect of leakage past the aileron nose on the aerodynamic characteristics of ailerons. Plain and internally balanced ailerons of 0.20 airfoil chord were tested on an NACA 66(215)-216, a-1.0 airfoil. The effects of amount and type of leakage, aileron contour, and Mach number and Reynolds number were investigated. The results of the tests indicated that a small amount of leakage area changed the pressure distributions over the plain and internally balanced ailerons markedly. This change generally resulted in negative increments in the lift and hinge-moment parameters c [subscript l] subscript [delta], c [subscript h] subscript [alpha], and c [subscript h] subscript [delta]. A further increase in the leakage area produced smaller changes in these parameters for the internally balanced aileron.

Author : K. R. Czarnecki
Publisher :
ISBN 13 :
Total Pages : 124 pages
Book Rating : 4.96/5 ( download)

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Download or read book Span Loadings and Aerodynamic Characteristics for a Series of Tip and Trailing-edge Controls on a 60° Delta Wing at Mach Numbers of 1.61 and 2.01 written by K. R. Czarnecki and published by . This book was released on 1959 with total page 124 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Author : J. Wayne Keyes
Publisher :
ISBN 13 :
Total Pages : 34 pages
Book Rating : 4.48/5 ( download)

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Download or read book Calculated and Experimental Hinge Moments on a Trailing-edge Flap of a 75° Swept Delta Wing at Mach 6 written by J. Wayne Keyes and published by . This book was released on 1967 with total page 34 pages. Available in PDF, EPUB and Kindle. Book excerpt: