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Experiments With A Wing Model From Which The Boundary Is Removed By Suction
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Book Synopsis Experiments with a Wing Model from which the Boundary is Removed by Suction by : Oskar Schrenk
Download or read book Experiments with a Wing Model from which the Boundary is Removed by Suction written by Oskar Schrenk and published by . This book was released on 1929 with total page 628 pages. Available in PDF, EPUB and Kindle. Book excerpt: The present report deals with a series of tests made for the purpose of improving flow conditions about wings by applying the suction principle (increase of the lift coefficient and reduction of the drag about very thick wing sections). Though not conclusive, the report contains interesting results.
Book Synopsis Experiments with an Airfoil Model on which the Boundary Layer is Controlled Without the Use of Supplementary Equipment by : I. H. Abbott
Download or read book Experiments with an Airfoil Model on which the Boundary Layer is Controlled Without the Use of Supplementary Equipment written by I. H. Abbott and published by . This book was released on 1931 with total page 16 pages. Available in PDF, EPUB and Kindle. Book excerpt: This report describes tests to determine the possibility of controlling the boundary layer on the upper surface of an airfoil by use of the low pressure existing near the leading edge. The low pressure was used to induce flow through slots in the upper surface of the wing. The tests showed that the angle of attack for maximum lift was increased at the expense of a reduction in the maximum lift coefficient and an increase in the drag coefficient.
Book Synopsis Experiments with a Wing from which the Boundary Layer is Removed by Suction by : Oskar Schrenk
Download or read book Experiments with a Wing from which the Boundary Layer is Removed by Suction written by Oskar Schrenk and published by . This book was released on 1931 with total page 12 pages. Available in PDF, EPUB and Kindle. Book excerpt: This report presents the results of the first investigation of the physical principle of preventing the streamline separation by removing the boundary layer. It was aeronautical, in that it dealt with airfoils, but the results are of a very general application.
Book Synopsis Wind Tunnel Tests on Airfoil Boundary Layer Control Using a Backward-opening Slot by : C. H. Dearborn
Download or read book Wind Tunnel Tests on Airfoil Boundary Layer Control Using a Backward-opening Slot written by C. H. Dearborn and published by . This book was released on 1931 with total page 160 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Experiments with a Wing from which the Boundary Layer is Removed by Pressure Or Suction by : K. Wieland
Download or read book Experiments with a Wing from which the Boundary Layer is Removed by Pressure Or Suction written by K. Wieland and published by . This book was released on 1928 with total page 14 pages. Available in PDF, EPUB and Kindle. Book excerpt: With an unsymmetrical wing and a rotating Magnus cylinder, the lift is produced by the superposition of parallel and circulatory flows. An explanation of the circulatory flow is furnished by the boundary-layer theory of Prandtl and the consequent vortex formation. According to this explanation, it must evidently be possible to increase the circulation either by increasing the size of the stronger (lower) vortex or by decreasing the size of the weaker (upper) vortex. In this sense, according to Professor H. Zickendraht, we have a new type of wing from which the boundary layer is removed by forcing air out or sucking it in through openings in the upper surface of the wing near its trailing edge.
Book Synopsis Tests in the Variable Density Wind Tunnel to Investigate the Effects of Scale and Turbulence on Airfoil Characteristics by : John Stack
Download or read book Tests in the Variable Density Wind Tunnel to Investigate the Effects of Scale and Turbulence on Airfoil Characteristics written by John Stack and published by . This book was released on 1931 with total page 556 pages. Available in PDF, EPUB and Kindle. Book excerpt: The effects of scale and turbulence on the lift and drag of five airfoils, the N.A.C.A. 0006 , the N.A.C.A. 0021, the Clark Y, The U.S.A 35-A, and the U.S.N. P.S.6, hve been investigated in the Variable Density Wind Tunnel. Tests were made over a wide scale for only two different conditions of turbulence.
Book Synopsis Theory of Wing Sections by : Ira H. Abbott
Download or read book Theory of Wing Sections written by Ira H. Abbott and published by Courier Corporation. This book was released on 2012-04-26 with total page 708 pages. Available in PDF, EPUB and Kindle. Book excerpt: Concise compilation of subsonic aerodynamic characteristics of NACA wing sections, plus description of theory. 350 pages of tables.
Book Synopsis Index of NACA Technical Publications by : United States. National Advisory Committee for Aeronautics
Download or read book Index of NACA Technical Publications written by United States. National Advisory Committee for Aeronautics and published by . This book was released on 1949 with total page 616 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Report by : United States. National Advisory Committee for Aeronautics
Download or read book Report written by United States. National Advisory Committee for Aeronautics and published by . This book was released on 1957 with total page 160 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Download or read book Technical Note written by and published by . This book was released on with total page 626 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Index of NACA Reports Having Application to Personal Aircraft by : United States. National Advisory Committee for Aeronautics
Download or read book Index of NACA Reports Having Application to Personal Aircraft written by United States. National Advisory Committee for Aeronautics and published by . This book was released on 1946 with total page 32 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Technical Note - National Advisory Committee for Aeronautics by : United States. National Advisory Committee for Aeronautics
Download or read book Technical Note - National Advisory Committee for Aeronautics written by United States. National Advisory Committee for Aeronautics and published by . This book was released on 1948 with total page 936 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis A Selected Listing of NASA Scientific and Technical Reports for ... by :
Download or read book A Selected Listing of NASA Scientific and Technical Reports for ... written by and published by . This book was released on 1949 with total page 664 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Report - National Advisory Committee for Aeronautics by : United States. National Advisory Committee for Aeronautics
Download or read book Report - National Advisory Committee for Aeronautics written by United States. National Advisory Committee for Aeronautics and published by . This book was released on 1928 with total page 532 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Technical Memorandums by : United States. National Advisory Committee for Aeronautics
Download or read book Technical Memorandums written by United States. National Advisory Committee for Aeronautics and published by . This book was released on 1929 with total page 540 pages. Available in PDF, EPUB and Kindle. Book excerpt: Chiefly translations from foreign aeronautical journals.
Download or read book NASA Technical Note written by and published by . This book was released on 1976 with total page 640 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Download or read book Report written by and published by . This book was released on 1957 with total page 1180 pages. Available in PDF, EPUB and Kindle. Book excerpt:
