Download or read book The Characteristics of 78 Related Airfoil Section from Tests in the Variable density Wind Tunnel written by Eastman Nixon Jacobs and published by . This book was released on 1933 with total page 190 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Download or read book The Characteristics of 78 Related Airfoil Sections from Tests in the Variable density Wind Tunnel written by Eastman N. Jacobs and published by . This book was released on 1933 with total page 64 pages. Available in PDF, EPUB and Kindle. Book excerpt: An investigation of a large group of related airfoils was made in the N.A.C.A. variable-density wind tunnel at a large value of the Reynolds Number. The tests were made to provide data that may be directly employed for a rational choice of the most suitable airfoil section for a given application. The variation of the aerodynamic characteristics with variations in thickness and mean-line form were therefore systematically studied.
Download or read book The Characteristics of 78 Related Airfoil Sections from Tests in the Variable density Wind Tunnel written by Eastman Nixon Jacobs and published by . This book was released on 1933 with total page 58 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Download or read book Tests in the Variable density Wind Tunnel Related Airfoils Having the Maximum Camber Unusually Far Forward written by A. M. Rothrock and published by . This book was released on 1935 with total page 194 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Download or read book Airfoil Section Data Obtained in the N A C A Variable density Tunnel as Affected by Support Interference and Other Corrections written by Eastman Nixon Jacobs and published by . This book was released on 1939 with total page 44 pages. Available in PDF, EPUB and Kindle. Book excerpt:
- Author : Isadore Edward Garrick
- Publisher :
- Release : 1938
- ISBN :
- Pages : 72 pages
Aerodynamic Characteristics of a Large Number of Airfoils Tested in the Variable density Wind Tunnel
Download or read book Aerodynamic Characteristics of a Large Number of Airfoils Tested in the Variable density Wind Tunnel written by Isadore Edward Garrick and published by . This book was released on 1938 with total page 72 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Download or read book Tests of N A C A Airfoils in the Variable density Wind Tunnel written by Eastman Nixon Jacobs and published by . This book was released on 1932 with total page 19 pages. Available in PDF, EPUB and Kindle. Book excerpt: This note is the fifth of a series covering an investigation of a number of related airfoils. It presents the results obtained from tests of a group of six low-cambered airfoils in the variable density wind tunnel. The mean camber lines are identical for the six airfoils and are of such a form that the maximum mean camber is 2 percent of the chord and is a position 0.4 of the chord behnid the leading edge. The airfoils differ in thickness only, the maximum-thickness/chord ratios being ).06, 0.09, 0.12, 0.15, 0.18, and 0.21. The results have been presented in the form of both infinite and finite aspect-ratio characteristics. The values for this group of airfoils are among the highest thus far obtained, the minimum profile drags being approximately equal to those for the symmetrical series of corresponding thickness, while the maximum lift coefficients are considerably higher.
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.
Download or read book Report written by United States. National Advisory Committee for Aeronautics and published by . This book was released on 1944 with total page 42 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Download or read book Wind tunnel Investigation of Tapered Wings with Ordinary Ailerons and Partial span Split Flaps written by Abe Silverstein and published by . This book was released on 1937 with total page 76 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Download or read book Annual Report National Advisory Committee for Aeronautics written by United States. National Advisory Committee for Aeronautics and published by . This book was released on 1945 with total page pages. Available in PDF, EPUB and Kindle. Book excerpt: Includes the Committee's Technical reports no. 1-1058, reprinted in v. 1-37.
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 1933 with total page 658 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Download or read book Tests of Related Forward camber Airfoils in the Variable density Wind Tunnel written by Eastman Nixon Jacobs and published by . This book was released on 1939 with total page 52 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Download or read book The Aerodynamic Characteristics of Seven Frequently Used Wing Sections at Full Reynolds Number written by Walter Stuart Diehl and published by . This book was released on 1926 with total page 208 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Download or read book Pressure Distribution Over a Clark Y H Airfoil Section with a Split Flap written by Carl J. Wenzinger and published by . This book was released on 1937 with total page 508 pages. Available in PDF, EPUB and Kindle. Book excerpt: An investigation was made in the N.A.C.A. 7- by 10-foot wind tunnel of the distributions of air pressure over one chord section of the Clark Y-H airfoil with a split flap. The results obtained are given in the form of diagrams showing the chordwise distribution of pressure on both airfoil and flap and as plots of calculated aerodynamic coefficients for both airfoil and flap.
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:
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: