Download or read book Wind Tunnel Tests on a 6 Two dimensional Aerofoil in the Transonic Speed Range written by P. E. Turner and published by . This book was released on 1956 with total page 18 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Download or read book Transonic Wind Tunnel Tests on a Series of Two dimensional Aerofoils in a Solid Wall Test Section written by B. D. Fairlie and published by . This book was released on 1979 with total page 12 pages. Available in PDF, EPUB and Kindle. Book excerpt: Transonic wind tunnel tests are reported on a series of two-dimensional models in a test section equipped with four solid walls. The tests were conducted on two geometrically similar models of each of two aerofoil sections -- NACA-0012 and BGK-1 -- and covered a range of Mach numbers between 0.5 and 0.82. The main purpose of the tests was to provide a body of data suitable for testing the validity of linear interference theory without the complication of the unknown boundary conditions associated with non-solid wind tunnel walls. (Author).

Download or read book Transonic Wind Tunnel Tests on Two dimensional Aerofoil Sections written by Georan Ehn and published by . This book was released on 1977 with total page 138 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Download or read book Transonic Wind Tunnel Testing written by B. H. Goethert and published by . This book was released on 2007 with total page 420 pages. Available in PDF, EPUB and Kindle. Book excerpt: Numerous aspects of transonic aerodynamics include wall interference corrections in conventional wind tunnels, subsonic flow in a variety of wind tunnels, and test results from transonic wind tunnels. 1961 edition.

Download or read book Two Dimensional Transonic Wind Tunnel Tests of Three 15 Percent Thick Circulation Control Airfoils written by Robert J. Englar and published by . This book was released on 1970 with total page 72 pages. Available in PDF, EPUB and Kindle. Book excerpt: Two-dimensional transonic wind tunnel tests were conducted on three fifteen percent circulation control elliptic airfoils over the Mach no. range 0.3 to 0.9. Model configurations included a pure elliptical shape with both jet flap and tangential upper surface trailing edge blowing, plus tangential blowing over an elliptical shape with a rounded trailing edge. Performance of the rounded trailing edge configuration was the best of the three at low speeds, but above M = 0.55, detachment of the Coanda jet caused rapid performance deterioration. Due to its elongated trailing edge and associated larger effective radius downstream of the slot, the tangentially blown pure ellipse was able to extend the jet detachment Mach number to 0.7, where maximum equivalent lift-to-drag ratios of 22 at a two-dimensional lift coefficient of 0.44 were achieved. The jet flaps proved to be inferior to the tangentially blown configurations in all respects except in its ability as a thrusting, drag-reducing body. (Author).

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:

Download or read book Scientific and Technical Aerospace Reports written by and published by . This book was released on 1995 with total page 704 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Download or read book Wind Tunnel Tests on a 6 Two dimensional Aerofoil with 25 Chord Flap written by P. E. Turner and published by . This book was released on 1957 with total page 20 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Download or read book Two Dimensional Aerofoil Section Tests on N P L Aerofoil A in the B A C 4 X 4 High Speed Wind Tunnel written by S. A. M. Thornley and published by . This book was released on 1966 with total page 28 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Download or read book An Experimental Investigation Into the General Application of Wind Tunnel Wall Corrections in Transonic Two dimensional Aerofoil Tests written by M. C. Lewis and published by . This book was released on 1995 with total page pages. Available in PDF, EPUB and Kindle. Book excerpt:

Download or read book Applied Mechanics Reviews written by and published by . This book was released on 1972 with total page 542 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Download or read book NRCL written by National Research Council Canada and published by . This book was released on 1974 with total page 170 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Download or read book Technical Abstract Bulletin written by and published by . This book was released on with total page 850 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Download or read book Centennial of Powered Flight written by G. M. Faeth and published by AIAA. This book was released on 2003 with total page 400 pages. Available in PDF, EPUB and Kindle. Book excerpt: Read it! Click on the paper titles below for a FREE preview of the content. This book contains papers written by the most remarkable minds in the field of aerospace over the past 60 years. It contains unusually significant papers that have appeared in the "AIAA Journal" and its predecessors ("Journal of Aeronautical Sciences, Journal of Aerospace Sciences, ARS Journal, ARS Bulletin, Astronautics, Journal of the American Rocket Society, " and "Jet Propulsion").

Download or read book The Status of Analytical Preparation for 2 dimensional Testing at High Transonic Speeds in the University of Southampton Transonic Self streamlining Wind Tunnel written by and published by . This book was released on 1984 with total page 32 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Download or read book Report written by North Atlantic Treaty Organization. Advisory Group for Aerospace Research and Development and published by . This book was released on 1960 with total page 774 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Download or read book Two dimensional Wind tunnel Tests of a NASA Supercritical Airfoil with Various High lift Systems Volume 2 Test Data written by and published by . This book was released on 1977 with total page 246 pages. Available in PDF, EPUB and Kindle. Book excerpt: