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 Investigation at Transonic Speeds of Loading Over a 30 Deg Sweptback Wing of Aspect Ratio 3 Taper Ratio 0 2 and NACA 65A004 Airfoil Section Mounted on a Body written by Donald D. Arabian and published by . This book was released on 1960 with total page 88 pages. Available in PDF, EPUB and Kindle. Book excerpt: The aerodynamic load characteristics of a wing-body combination were determined experimentally at Mach numbers from 0.80 to 1.03 for angles of attack up to 26 degrees. Two wings, both with 30 degrees sweep of the quarter-chord line, taper ratio of 0.2, aspect ratio of 3, and thickness of 4 percent chord, but of different types of construction, were tested. One wing was of solid steel and the other was of plastic with an inner steel core ...
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 An Investigation at Transonic Speeds of the Effects of Thickness Ratio and of Thickened Root Sections on the Aerodynamic Characteristics of Wings with 47 Sweepback Aspect Ratio 3 5 and Taper Ratio 0 2 in the Slotted Test Section of the Langley 8 foot High speed Tunnel written by Ralph P. Bielat and published by . This book was released on 1951 with total page 44 pages. Available in PDF, EPUB and Kindle. Book excerpt: Four wing-body combinations of the same plan form (47 degree sweep, 3.5 aspect ratio, and 0.2 taper ratio) were compared at transonic speeds in the Langley 8-foot high-speed tunnel. Three wings were 4, 6, and 9 percent thick; the fourth was 6 percent thick but, on the inner 0.4 span, tapered to 12-percent thickness at the roots.
Download or read book Apollo Program Summary Report written by and published by . This book was released on 1975 with total page 526 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 The Apollo Spacecraft Ertel I D and Morse M L Through November 7 1962 written by Ivan D. Ertel and published by . This book was released on 1969 with total page 292 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Download or read book Aerodynamic Characteristics of Low aspect ratio Wings in Close Proximity to the Ground written by Marvin P. Fink and published by . This book was released on 1961 with total page 44 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Download or read book Flight Investigation of an Aileron and a Spoiler on a Wing of the X 3 Airplane Plan Form at Mach Numbers from 0 5 to 1 6 written by Roland D. English and published by . This book was released on 1954 with total page 20 pages. Available in PDF, EPUB and Kindle. Book excerpt:
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 Wind tunnel Investigation at Low Speed of Lateral Control Characteristics of an Untapered 45 Sweptback Semispan Wing of Aspect Ratio 1 59 Equipped with Various 25 percent chord Plain Ailerons written by Harold S. Johnson and published by . This book was released on 1951 with total page 38 pages. Available in PDF, EPUB and Kindle. Book excerpt: A wind-tunnel investigation at low speed was made to determine the lateral control characteristics of a 45 degree sweptback untapered semispan wing of aspect ratio 1.59 equipped with various 25-percent-chord plain unsealed ailerons. Variations of the lateral-control data with aileron span and spanwise location were determined through a large aileron-deflection range for various angles of attack up to about the angle of maximum lift.
Download or read book Discover aeronautics and space written by and published by . This book was released on 1990 with total page 28 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Download or read book Aerodynamic center Considerations of Wings and Wing body Combinations written by John E. Lamar and published by . This book was released on 1966 with total page 20 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Download or read book Aerodynamic Loads on an Isolated Shrouded propeller Configuration of Angles of Attack from 10 Degrees to 110 Degrees written by Kalman J. Grunwald and published by . This book was released on 1962 with total page 36 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Download or read book An Accelerated Reservoir Light gas Gun written by John S. Curtis and published by . This book was released on 1962 with total page 28 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Download or read book Aeronautical and Astronautical Events of 1961 written by United States. National Aeronautics and Space Administration and published by . This book was released on 1962 with total page 124 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Download or read book A 6 inch Subsonic High temperature Arc Tunnel for Structures and Material Tests written by Ronald D. Brown and published by . This book was released on 1963 with total page 40 pages. Available in PDF, EPUB and Kindle. Book excerpt:
