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 286 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 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 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 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 Technical Abstract Bulletin written by Defense Documentation Center (U.S.) and published by . This book was released on 1961-02 with total page 1116 pages. Available in PDF, EPUB and Kindle. Book excerpt:
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 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 1 pages. Available in PDF, EPUB and Kindle. Book excerpt: An investigation was conducted at the Langley 16-foot transonic tunnel to determine the loading characteristics of flap-type 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, at angles of attack up to about 27 degrees, and at aileron deflections between approximately -15 degrees and 15 degrees. Results of the investigation indicate that the loading over the ailerons was established by the wing-flow characteristics, and the loading shapes were irregular in the transonic speed range. The spanwise location of the aileron had little effect on the values of the slope of the curves of hinge-moment coefficient against aileron deflection, but the inboard aileron had the greatest value of the slope of curves of hinge-moment coefficient against angle of attack and the outboard aileron had the least. Hinge-moment and aileron normal-force data taken with strain-gage instrumentation are compared with data obtained with pressure measurements. (Author).
Download or read book Battelle Technical Review written by Battelle Memorial Institute and published by . This book was released on 1961 with total page 830 pages. Available in PDF, EPUB and Kindle. Book excerpt:
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 Loads on Thin Wings at Transonic Speeds written by Don D. Davis (Jr.) and published by . This book was released on 1955 with total page 22 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Download or read book Loads on Wings Due to Spoilers at Subsonic and Transonic Speeds written by Alexander D. Hammond and published by . This book was released on 1955 with total page 18 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 Some Effects of External Wing Tip Stores on the Rolling Effectiveness and Drag of Plain and Half delta Tip Ailerons on a 4 percent thick Tapered Unswept Wing written by Roland D. English and published by . This book was released on 1954 with total page 22 pages. Available in PDF, EPUB and Kindle. Book excerpt: The Langley Pilotless Aircraft Research Division has made an investigation to determine some effects of external wing tip tanks on the rolling effectiveness and drag of plain and half-delta tip ailerons on a 4-percent-thick, tapered, unswept wing. The investigation was made by means of a rocket-propelled models in free flight over a range of Mach numbers from 0.6 to 1.5.
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 Lateral control Investigation at Transonic Speeds of Differentially Deflected Horizontal tail Surfaces for a Configuration Having a 6 percent thick 45 Degrees Sweptback Wing written by Chris C. Critzos and published by . This book was released on 1956 with total page pages. Available in PDF, EPUB and Kindle. Book excerpt:
