Span Loadings And Aerodynamic Characteristics For A Series Of Tip And Trailing Edge Controls On A 60 Delta Wing At Mach Numbers Of 161 And 201

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 : Emma Jean Landrum
Publisher :
ISBN 13 :
Total Pages : 82 pages
Book Rating : 4.20/5 ( download)

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Download or read book Spanwise Loadings and Aerodynamic Characteristics for a Series of Trailing-edge Controls on a 40° Sweptback Wing at Mach Numbers of 1.61 and 2.01 written by Emma Jean Landrum and published by . This book was released on 1962 with total page 82 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 : 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 : 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 : 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 :
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ISBN 13 :
Total Pages : 40 pages
Book Rating : 4.81/5 ( download)

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Download or read book Effects of External Stores on the Aerodynamic Characteristics of a 60 Deg Delta-wing Fighter Model at Mach 1.60 to 2.87 written by and published by . This book was released on 1977 with total page 40 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Author : Emma Jean Landrum
Publisher :
ISBN 13 :
Total Pages : 70 pages
Book Rating : 4.83/5 ( download)

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Download or read book Pressure Distributions and Aerodynamic Characteristics of Several Spoiler Controls on a 40 Degree Sweptback Wing at a Mach Number of 1.61 written by Emma Jean Landrum and published by . This book was released on 1960 with total page 70 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Author : Frederick C. Grant
Publisher :
ISBN 13 :
Total Pages : 18 pages
Book Rating : 4.10/5 ( download)

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Download or read book Span Loadings Due to Wing Twist at Transonic and Supersonic Speeds written by Frederick C. Grant and published by . This book was released on 1957 with total page 18 pages. Available in PDF, EPUB and Kindle. Book excerpt: Two similar tapered sweptback plan forms with the same two spanwise variations of twist have been tested in the Mach number range from 0.8 to 2.0. The test results showed, in general, rather good agreement with theoretical predictions of the incremental span loadings due to twist for zero angle of attack. The measured incremental span loadings due to twist generally diminished with increasing angle of attack through the Mach number range. At a Mach number of 0.9, the incremental loadings progressively vanished from the tip inboard with increasing angle of attack. For the highest angles of attack (about 20 degrees) at Mach number 0.9, there was no difference in the span loadings of the flat and twisted wings. At a higher supersonic speeds, a similar vanishing at the tips of the incremental loading due to twist was starting at the highest angles of attack (near 20 degrees).

Author : Robert S. Osborne
Publisher :
ISBN 13 :
Total Pages : 20 pages
Book Rating : 4.25/5 ( download)

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Download or read book A Note on the Drag Due to Lift of Delta Wings at Mach Numbers Up to 2.0 written by Robert S. Osborne and published by . This book was released on 1960 with total page 20 pages. Available in PDF, EPUB and Kindle. Book excerpt: