Download or read book Investigation of Wing tip Ailerons on a 51 3 Degrees Sweptback Wing at Transonic Speeds by the Transonic bump Method written by William C. Jr Moseley and published by . This book was released on 1951 with total page 60 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Download or read book Research Abstracts and Reclassification Notice written by United States. National Advisory Committee for Aeronautics and published by . This book was released on 1954 with total page 508 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Download or read book Research Abstracts written by United States. National Advisory Committee for Aeronautics and published by . This book was released on with total page 442 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Download or read book Lateral control Investigation at Transonic Speeds of Retractable Spoiler and Plug type Spoiler slot Ailerons on a Tapered 60 Degree Sweptback Wing of Aspect Ratio 2 written by Alexander D. Hammond and published by . This book was released on 1952 with total page 19 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Download or read book Preliminary Investigation of Various Ailerons on a 42 Degrees Sweptback Wing for Lateral Control at Transonic Speeds written by Thomas R. Turner and published by . This book was released on 1948 with total page 35 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Download or read book Investigation at Transonic Speeds of the Loading Over a 45 Degree Sweptback Wing Having an Aspect Ratio of 3 a Taper Ratio of 0 2 and NACA 65A004 Airfoil Sections written by Jack F. Runckel and published by . This book was released on 1956 with total page 104 pages. Available in PDF, EPUB and Kindle. Book excerpt: An investigation at transonic speeds of the loading over a 45 degree sweptback wing having an aspect ratio of 3, a taper ratio of 0.2, and NACA 65A004 airfoil sections has been conducted in the Langley16-foot transonic tunnel. Pressure measurements on the wing-body combination were obtained at angles of attack from 0 to 26 degrees at Mach numbers from 0.80 to 0.98 and from 0 to about 12 degrees at Mach numbers from 1.00 to 1.05. Reynolds number, based on the wing mean aerodynamic chord, varied from 7,000,000 to 8,500,000 over the test Mach number range.

Download or read book An Investigation of Wing and Aileron Loads Due to Deflected Inboard and Outboard Ailerons on a 4 percent thick 30 Degree Swepptback Wing at Transonic Speeds written by Charles F. Whitcomb and published by . This book was released on 1961 with total page 286 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Download or read book Free flight Investigation at Transonic and Supersonic Speeds of the Rolling Effectiveness of a 42 7 Degree Sweptback Wing Having Partial span Ailerons written by Carl A. Sandahl and published by . This book was released on 1948 with total page 13 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Download or read book An Investigation of Wing and Alleron Loads Due to Deflected Inboard and Outboard Ailerons on a 4 percent thick 30 Degrees Sweptback Wing at Transonic Speeds written by Charles F. Whitcomb and published by . This book was released on 1961 with total page 282 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Download or read book Investigation of Wing Flutter at Transonic Speeds for Six Systematically Varied Wing Plan Forms written by George W. Jones and published by . This book was released on 1953 with total page 40 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Download or read book Aerodynamic Characteristics at Transonic Speeds of a Tapered 45 Degree Sweptback Wing of Aspect Ratio 3 Having a Full span Flap Type of Control with Overhang Balance written by Vernard E. Lockwood and published by . This book was released on 1952 with total page 24 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Download or read book Investigation of Transonic Flutter Characteristics of a Thin 10 Degree Sweptback Wing Having an Aspect Ratio of 4 and a Taper Ratio of 0 6 written by George W. Jones and published by . This book was released on 1957 with total page 22 pages. Available in PDF, EPUB and Kindle. Book excerpt: A flutter investigation has been made in the Langley transonic blowdown tunnel at Mach numbers between 0.79 and 1.34 on a thin 10 degree sweptback wing having an aspect ratio of 4 and a taper ratio of 0.6. The data obtained have been compared with data from NACA Research Memorandum L55I13A for zero and 30 degree sweptback wings of the type investigated, the flutter boundary for the 10 degree sweptback wing falls between those for the zero degree and 30 degree sweptback wings in the low supersonic Mach number range. However, the subsonic level (around a Mach number of 0.8) of the flutter boundary for the 10 degree sweptback wing lies above those for the zero and 30 degree sweptback wings. In addition, the amount of rise in the flutter boundary from the subsonic level to the supersonic values is about the same for the wings with angles of sweepback of 10 degrees and zero degrees, but is much greater for the wing with an angle of sweepback of 30 degrees.

Download or read book A Wind tunnel Investigation of the Wing Loads Due to Deflected Inboard Ailerons on a 45 Degree Sweptback Wing at Transonic Speeds written by Astwood R. Jr Heath and published by . This book was released on 1958 with total page 100 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Download or read book Investigation of Three Tapered 45 Degree Sweptback Cambered and Twisted Wings Covering a Simultaneous Variation in Aspect Ratio and Thickness Ratio and of One Related Symmetrical Wing at Transonic Speeds by the Wing flow Method written by Harold I. Johnson and published by . This book was released on 1953 with total page 55 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Download or read book Aerodynamic Characteristics at Transonic Speeds of a Tapered 45 Degrees Sweptback Wing of Aspect of Aspect Ratio 3 Having a Full span Flap tyre Control written by Vernard E. Lockward and published by . This book was released on 1951 with total page 35 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Download or read book Investigation of the Effects of Twist and Camber on the Aerodynamic Characteristics of a 50 degrees 38 Sweptback Wing of Aspect Ratio 2 98 written by Kenneth P. Spreemann and published by . This book was released on 1951 with total page 30 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Download or read book Flight Investigation to Determine the Hinge Moments of a Beveled edge Aileron on a 45 Degree Sweptback Wing at Transonic and Low Supersonic Speeds written by William N. Gardner and published by . This book was released on 1947 with total page 20 pages. Available in PDF, EPUB and Kindle. Book excerpt: