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Author : O. Knappe
Publisher :
ISBN 13 :
Total Pages : pages
Book Rating : 4.:/5 (11 download)
Download or read book High Speed Wind Tunnel Tests on a Symmetrical Wing with Flaps written by O. Knappe and published by . This book was released on 1947 with total page pages. Available in PDF, EPUB and Kindle. Book excerpt:
Author : Michael S. Selig
Publisher : Soartech
ISBN 13 :
Total Pages : 320 pages
Book Rating : 4.F/5 ( download)
Download or read book Summary of Low Speed Airfoil Data written by Michael S. Selig and published by Soartech. This book was released on 1995 with total page 320 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Author : Jerry V. Kirk
Publisher :
ISBN 13 :
Total Pages : 44 pages
Book Rating : 4.:/5 (31 download)
Download or read book Large-scale Wind-tunnel Investigation of a Model with an External Jet-augmented Flap written by Jerry V. Kirk and published by . This book was released on 1967 with total page 44 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Author : Anthony M. Cook
Publisher :
ISBN 13 :
Total Pages : 66 pages
Book Rating : 4.:/5 (31 download)
Download or read book Results of Full-scale Wind Tunnel Tests on the H.126 Jet Flap Aircraft written by Anthony M. Cook and published by . This book was released on 1969 with total page 66 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Author : Alan Pope
Publisher :
ISBN 13 :
Total Pages : 542 pages
Book Rating : 4.:/5 (89 download)
Download or read book Wind-tunnel Testing written by Alan Pope and published by . This book was released on 1954 with total page 542 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Author : Fred E. Weick
Publisher :
ISBN 13 :
Total Pages : 4 pages
Book Rating : 4.:/5 (25 download)
Download or read book Wind-tunnel Tests of a Hall High-lift Wing written by Fred E. Weick and published by . This book was released on 1932 with total page 4 pages. Available in PDF, EPUB and Kindle. Book excerpt: Wind-tunnel tests have been made to find the lift, drag, and center-of -pressure characteristics of a Hall high-lift wing model. The Hall wing is essentially a split-flap airfoil with an internal air passage. Air enters the passage through an opening in the lower surface somewhat back of and parallel to the leading edge and flows out through an opening made by deflecting the rear portion of the under surface downard as a flapl. For ordinary flight conditions the fornt opening and the rear flap can be closed, providing in effect a conventional airfoil. The tests were made with various flap settings and with the entrance to the passage both open and closed,. The highest lift coefficient found was obtained with the passage closed.
Author : Nigel GREGORY
Publisher :
ISBN 13 :
Total Pages : 16 pages
Book Rating : 4.:/5 (31 download)
Download or read book Wind-Tunnel Tests on the 30 Per Cent. Symmetrical Griffith Aerofoil with Ejection of Air at the Slots. By N. Gregory ... W. S. Walker and W. G. Raymer written by Nigel GREGORY and published by . This book was released on 1952 with total page 16 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Author : Kiyoshi Aoyagi
Publisher :
ISBN 13 :
Total Pages : 64 pages
Book Rating : 4.:/5 (31 download)
Download or read book Large-scale Wind-tunnel Tests in Ground Effect of a 35 ̊sweptback Wing Jet Transport Model Equipped with Blowing Boundary-layer-control Trailing-and Leading-edge Flaps written by Kiyoshi Aoyagi and published by . This book was released on 1963 with total page 64 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Author : Wallace H. Deckert
Publisher :
ISBN 13 :
Total Pages : 46 pages
Book Rating : 4.:/5 (31 download)
Download or read book Large-scale Wind-tunnel Tests of Descent Performance of an Airplane Model with a Tilt Wing and Differential Propeller Thrust written by Wallace H. Deckert and published by . This book was released on 1964 with total page 46 pages. Available in PDF, EPUB and Kindle. Book excerpt: Tests were conducted to determine the wing stall, performance, and longitudinal stability and control characteristics of a large model of a V/STOL tilt-wing transport aircraft. The scope of the tests was limited primarily to the low-speed transitional regime.
Author : J. J. Kacprzynski
Publisher :
ISBN 13 :
Total Pages : 480 pages
Book Rating : 4.:/5 (455 download)
Download or read book Wind Tunnel Tests of a Boerstoel Shockless Symmetrical Airfoil 0.11-0.75-1.375 written by J. J. Kacprzynski and published by . This book was released on 1972 with total page 480 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Author :
Publisher :
ISBN 13 :
Total Pages : 32 pages
Book Rating : 4.:/5 (317 download)
Download or read book Large-scale Wind-tunnel Tests at Low Speed of a Delta Winged Supersonic Transport Model in the Presence of the Ground written by and published by . This book was released on 1962 with total page 32 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Author : James A. Weiberg
Publisher :
ISBN 13 :
Total Pages : 38 pages
Book Rating : 4.:/5 (31 download)
Download or read book Large-scale Wind-tunnel Tests of an Airplane Model with an Unswept, Tilt Wing of Aspect Ration 5.5, and with Four Propellers and Blowing Flaps written by James A. Weiberg and published by . This book was released on 1961 with total page 38 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Author :
Publisher :
ISBN 13 :
Total Pages : 376 pages
Book Rating : 4.:/5 (3 download)
Download or read book Scientific and Technical Aerospace Reports written by and published by . This book was released on 1995 with total page 376 pages. Available in PDF, EPUB and Kindle. Book excerpt: Lists citations with abstracts for aerospace related reports obtained from world wide sources and announces documents that have recently been entered into the NASA Scientific and Technical Information Database.
Author :
Publisher :
ISBN 13 :
Total Pages : 94 pages
Book Rating : 4.:/5 (317 download)
Download or read book Low Speed Wind Tunnel Tests on a One-seventh Scale Model of the H.126 Jet Flap Aircraft written by and published by . This book was released on 1975 with total page 94 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Author : David B. Stevenson
Publisher :
ISBN 13 :
Total Pages : 33 pages
Book Rating : 4.:/5 (249 download)
Download or read book High-speed Wind-tunnel Tests of an NACA 0009-64 Airfoil Having a 33.4-percent-chord Flap with an Overhang 20.1 Percent of the Flap Chord written by David B. Stevenson and published by . This book was released on 1947 with total page 33 pages. Available in PDF, EPUB and Kindle. Book excerpt: Tests were conducted to investigate the effects of compressibility on a 5-inch-chord NACA 0009-64 airfoil section having a 33.4-percent-chord flap with a nose overhang of 20.1 percent of the flap chord and a 0.017-percent-chord unsealed gap. Airfoil lift and pitching moment and flap hinge moment were obtained over an angle-of-attack range of 6 degrees and a flap-angle range of 16 degrees from a Mach number of 0.4 to the maximum (choking) Mach number that could be obtained for each configuration.
Author : Robert B. Liddell
Publisher :
ISBN 13 :
Total Pages : 94 pages
Book Rating : 4.3/5 (126 download)
Download or read book Wind-tunnel Investigation of Control-surface Characteristics written by Robert B. Liddell and published by . This book was released on 1944 with total page 94 pages. Available in PDF, EPUB and Kindle. Book excerpt: Summary: Wind-tunnel tests have been made in two-dimensional flow to investigate the aerodynamic characteristics of a double flap with an internal and an overhang balance. Three sizes of each type of balance were tested with three relative rates of deflection of the two flaps. An NACA 66-009 airfoil having a 0.30-airfoil-chord straight-contour forward flap and a 0.20-airfoil-chord straight-contour rearward flap was used. The test results indicated that a balanced double flap produced the same lift as a single plain flap of the same chord and also produced highly balanced hinge moments. High lifts and low hinge moments were obtained with a double-flap arrangement if either an overhang or an internal balance having a chord 50 percent of the flap chord was incorporated on the forward flap. The overhang-balance flap showed a lower value of the hinge-moment gradient due to flap deflection than the internally balanced flap.
Author : P.E. Turner
Publisher :
ISBN 13 :
Total Pages : 117 pages
Book Rating : 4.:/5 (11 download)
Download or read book High Speed Wind Tunnel Tests on a 6 Percent Two-dimensional Aerofoil with 25 Percent Chord Flap written by P.E. Turner and published by . This book was released on 1957 with total page 117 pages. Available in PDF, EPUB and Kindle. Book excerpt:
