Download or read book Transonic Characteristics of Outboard Ailerons on a 4 percent thick 30 Degree Sweptback Wing Including Some Effects of Aileron Trailing edge Thickness and Aerodynamic Balance written by Charles F. Whitcomb and published by . This book was released on 1958 with total page 70 pages. Available in PDF, EPUB and Kindle. Book excerpt:
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 Research Abstracts written by United States. National Advisory Committee for Aeronautics and published by . This book was released on 1951 with total page 568 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Download or read book Normal force and Hinge moment Characteristics at Transonic Speeds of Flap type Ailerons at Three Spanwise Locations on a 4 percent thick Sweptback wing body Model and Pressure distribution Measurements on an Inboard Aileron written by Jack F. Runckel and published by . This book was released on 1961 with total page 60 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Download or read book An Investigation of Wing and Aileron Loads Due to Deflected Inboard and Outboard Ailerons on a 4 Percent Thick 30 Deg Sweptback Wing at Transonic Speeds written by Charles F. Whitcomb and published by . This book was released on 1961 with total page pages. Available in PDF, EPUB and Kindle. Book excerpt:
Download or read book Investigation of a 42 7 Degree Sweptback Wing Model to Determine the Effects of Trailing edge Thickness on the Aileron Hinge moment and Flutter Characteristics at Transonic Speeds written by Robert F. Thompson and published by . This book was released on 1950 with total page 42 pages. Available in PDF, EPUB and Kindle. Book excerpt: An investigation was made in the Langley high-speed 7- by 10-foot tunnel of 42.7 degrees sweptback wing model to determine the effects of aileron trailing-edge thickness on aileron hinge moments and one-degree-of-freedom aileron flutter. The wing had an aspect ratio of 4.0, a taper ratio of 0.5, and was tested over a Mach number range of 0.60 to 1.175. The half-span, 20-percent-chord ailerons were flat sided and located outboard.
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 1951 with total page 596 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Download or read book Normal force and Hinge moment Characteristics at Transonic Speeds of Flap type Ailerons at Three Spanwise Locations on a 4 percent thick Sweptback wing body Model and Pressure Distribution Measurements on an Inboard Aileron written by Jack F. Runckel and published by . This book was released on 1957 with total page 55 pages. Available in PDF, EPUB and Kindle. Book excerpt: An investigation has been conducted at the Langley 16-foot transonic tunnel to determine the loading characteristics of flap-down ailerons located at inboard, midspan, and outboard positions on a 45 degree sweptback-wing-body combination. Aileron normal-force and hinge-moment data have been obtained at Mach numbers from 0.80 to 1.03, with angles of attack up to about 27 degrees, and at aileron deflections between approximately plus or minus 15 degrees.
Download or read book Effectiveness at Transonic Speeds of Flap type Ailerons for Several Spanwise Locations on a 4 percent Thick Swept back wing fuselage Model with and Without Tails written by Gerald Hieser and published by . This book was released on 1957 with total page 34 pages. Available in PDF, EPUB and Kindle. Book excerpt: A transonic investigation has been made in the Langley 16-foot transonic tunnel to determine the effects of spanwise location of a flap-type aileron on the lateral characteristics of a 4-percent-thick sweptback wing-fuselage model. Some effects of the model tail on the lateral characteristics are also included. The inboard, midspan, and outboard ailerons have a span of 40 percent of the wing semispan and a chord of 30 percent of the wing chord. The tests covered Mach numbers from 0.80 to 1.03 and angles of attack up to 27 degrees.
Download or read book Aerodynamic Characteristics at Subsonic and Transonic Speeds of a 42 7 Degrees Sweptback Wing Model Having an Aileron with Finite Trailing edge Thickness written by Thomas R. Turner and published by . This book was released on 1949 with total page 24 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Download or read book An Investigation of Wing and Aileron Loads Due to Deflected Inboard and Outboard Ailerons on a 4 percent thick 30 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 Effect of Full span Trailing edge Elevons on the Transonic Longitudinal Aerodynamic Characteristics of a Wing body Combination Having a 3 percent thick Triangular Wing with 60 Degree Leading edge Sweep written by Chris C. Critzos and published by . This book was released on 1957 with total page 29 pages. Available in PDF, EPUB and Kindle. Book excerpt: An investigation to determine the effects of full-span trailing-edge flaps on the static longitudinal characteristics of a triangular wing-body combination was conducted in the Langley 16-foot transonic tunnel. This wing had a leading-edge sweep of 60 degrees, an aspect ratio of 2.06, and NACA 65A003 airfoil sections. Force data were obtained for the basic configuration and for the wing with control surfaces deflected for longitudinal control through a deflection range of -15 to 7.5 degrees. Data were obtained at angles of attack generally from 0 degrees to as high as 26 degrees for Mach numbers ranging from 0.80 to 1.05. The Reynolds number varied from 9,800,000 to 10,500,000.
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 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 0 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Download or read book The Twisting Effect at Transonic Speeds of Spoiler Ailerons on a 45 Sweptback Aspect ratio 4 Tapered Wing written by Alexander D. Hammond and published by . This book was released on 1954 with total page 26 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 Flutter Characteristics of Swept Wings at Transonic Speeds written by Laurence K. Loftin and published by . This book was released on 1955 with total page 20 pages. Available in PDF, EPUB and Kindle. Book excerpt:
