Experimental Pressure Distributions Over Wing Tips At Mach Number 19
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Author | : Harold Mirels |
Publisher | : |
Total Pages | : 28 |
Release | : 1949 |
Genre | : Aerodynamic load |
ISBN | : |
Download Experimental Pressure Distributions Over Wing Tips at Mach Number 1.9 Book in PDF, Epub and Kindle
An investigation was conducted at a Mach number of 1.90 to determine spanwise pressure distribution over a wing tip in a region influenced by a sharp subsonic trailing edge. The wing section was a symmetrical wedge of 5 degrees 43 minutes total included angle in the free-stream direction. The investigation was conducted over a range of angles of attack from -10 to 10 degrees at a Reynolds number of 3,400,000 per foot.
Author | : Lowell E. Hasel |
Publisher | : |
Total Pages | : 120 |
Release | : 1959 |
Genre | : Aerodynamic load |
ISBN | : |
Download An Experimental Pressure-distribution Investigation of Interference Effects Produced at a Mach Number of 3.11 by Wedge- Shaped Bodies Located Under a Triangular Wing Book in PDF, Epub and Kindle
Author | : Henry C. Lessing |
Publisher | : |
Total Pages | : 98 |
Release | : 1960 |
Genre | : Aerodynamics, aircraft |
ISBN | : |
Download Experimental Determination of the Pressure Distribution on a Rectangular Wing Oscillating in the First Bending Mode for Mach Numbers from 0.24 to 1.30 Book in PDF, Epub and Kindle
Author | : Stavros A. Hartofilis |
Publisher | : |
Total Pages | : 68 |
Release | : 1963 |
Genre | : Aerodynamics, Hypersonic |
ISBN | : |
Download Pressure Measurement at Mach 19 for a Winged Re-entry Configuration Book in PDF, Epub and Kindle
Author | : Julio Chu |
Publisher | : |
Total Pages | : 44 |
Release | : 1996 |
Genre | : Angle of attack |
ISBN | : |
Download Experimental Surface Pressure Data Obtained on 65 ̊delta Wing Across Reynolds Number and Mach Number Ranges Book in PDF, Epub and Kindle
Author | : Cornelius Driver |
Publisher | : |
Total Pages | : 208 |
Release | : 1959 |
Genre | : Aerodynamic load |
ISBN | : |
Download Tabulated Data from a Pressure-distribution Investigation at Mach Number 2.01 of the Wing of a Canard Airplane Model Book in PDF, Epub and Kindle
Author | : |
Publisher | : |
Total Pages | : 122 |
Release | : 1959 |
Genre | : |
ISBN | : |
Download An Experimental Pressure-distribution Investigation of Interference Effects Produced at a Mach Number of 3.11 by Wedge- Shaped Bodies Located Under a Triangular Wing Book in PDF, Epub and Kindle
Author | : Thomas L. Fischetti |
Publisher | : |
Total Pages | : 98 |
Release | : 1957 |
Genre | : Aerodynamic load |
ISBN | : |
Download Investigation at Mach Numbers from 0.80 to 1.43 of Pressure and Load Distributions Over a Thin 45© Sweptback Highly Tapered Wing in Combination with Basic and Indented Bodies Book in PDF, Epub and Kindle
Pressure distributions have been obtained in the Langley 8-foot transonic tunnels over a Mach number range from 0.80 to 1.125 and at a Mach number of 1.43 for a 45 degree sweptback cambered wing having a thickened root, an aspect ratio of 4.0, and a taper ratio of 0.15. Data were obtained for the wing in the presence of a basic Sears-Haack body and a body indented symmetrically for a Mach number of 1.2.
Author | : Alberta Y. Alksne |
Publisher | : |
Total Pages | : 56 |
Release | : 1961 |
Genre | : Aerodynamics, Transonic |
ISBN | : |
Download Theoretical Pressure Distributions on Wings of Finite Span at Zero Incidence for Mach Numbers Near 1 Book in PDF, Epub and Kindle
Author | : Lannie D. Webb |
Publisher | : |
Total Pages | : 24 |
Release | : 1988 |
Genre | : |
ISBN | : |
Download Measured and Predicted Pressure Distributions on the AFTI/F-111 Mission Adaptive Wing Book in PDF, Epub and Kindle