Transonic Wind Tunnel Investigation Of The Low Lift Aerodynamic Characteristics Including The Effects Of Leading Edge Droop And Thickness Of A Thin Trapezoidal Wing In Combination With Basic And Indented Bodies PDF Download
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| Author | : Thomas C. Kelly |
| Publisher | : |
| Total Pages | : 29 |
| Release | : 1957 |
| Genre | : Aerodynamics |
| ISBN | : |
Download Transonic Wind-tunnel Investigation of the Low-lift Aerodynamic Characteristics, Including the Effects of Leading Edge Droop and Thickness, of a Thin Trapezoidal Wing in Combination with Basic and Indented Bodies Book in PDF, ePub and Kindle
An investigation has been conducted in the Langley 8-foot transonic tunnels to determine the aerodynamic force characteristics at low lift coefficients for a 2-percent-thick trapezoidal wing tested in combination with basic and indented bodies. Effects of wing leading-edge droop and wing thickness are included. Tests extended generally over a Mach number range from 0.80 to 1.43 and an angle-of-attack range from about 0.93 to 0.90.
| Author | : Thomas C. Kelly |
| Publisher | : |
| Total Pages | : 86 |
| Release | : 1957 |
| Genre | : Aerodynamic load |
| ISBN | : |
Download Transonic Wind-tunnel Investigation of Aerodynamic-loading Characteristics of a 2-percent-thick Trapezoidal Wing in Combination with Basic and Indented Bodies Book in PDF, ePub and Kindle
Pressure data have been obtained in the Langley 8-foot transonic tunnel at Mach numbers from 0.80 to 1.115 and angles of attack from 0 to 20 degrees for wing-body configurations employing a thin trapezoidal wing in combination with basic and indented bodies. The wing had 26.6 degrees sweepback of the quarter-chord line, an aspect ratio of 2.61, a taper ratio of 0.211, and 2-percent-thick symmetrical circular-arc airfoil sections parallel to the plane of symmetry. Results are also presented for the basic body alone. Reynolds numbers for the tests were on the order of 2,600,000, based on the wing mean aerodynamic chord.
| Author | : United States. National Aeronautics and Space Administration |
| Publisher | : |
| Total Pages | : 500 |
| Release | : 1959 |
| Genre | : Aeronautics |
| ISBN | : |
Download Index of NASA Technical Publications Book in PDF, ePub and Kindle
| Author | : United States. National Advisory Committee for Aeronautics |
| Publisher | : |
| Total Pages | : 388 |
| Release | : 1959 |
| Genre | : Aeronautics |
| ISBN | : |
Download Index of NACA Technical Publications Book in PDF, ePub and Kindle
| Author | : |
| Publisher | : |
| Total Pages | : 494 |
| Release | : 1959 |
| Genre | : Aeronautics |
| ISBN | : |
Download Index of NASA Technical Publications Book in PDF, ePub and Kindle
| Author | : |
| Publisher | : |
| Total Pages | : 388 |
| Release | : 1957 |
| Genre | : Aeronautics |
| ISBN | : |
Download A Selected Listing of NASA Scientific and Technical Reports for ... Book in PDF, ePub and Kindle
| Author | : United States. Superintendent of Documents |
| Publisher | : |
| Total Pages | : 1812 |
| Release | : 1960 |
| Genre | : Government publications |
| ISBN | : |
Download Monthly Catalog of United States Government Publications Book in PDF, ePub and Kindle
| Author | : United States. National Aeronautics and Space Administration |
| Publisher | : |
| Total Pages | : 300 |
| Release | : 1960 |
| Genre | : |
| ISBN | : |
Download Index to NASA Technical Publications Book in PDF, ePub and Kindle
| Author | : |
| Publisher | : |
| Total Pages | : 44 |
| Release | : 1959 |
| Genre | : |
| ISBN | : |
Download Aerodynamic Loading Characteristics Including Effects of Aeroelasticity of a Thin-Trapezoidal-Wing-Body Combination at Mach Number of 1.43 Book in PDF, ePub and Kindle
| Author | : |
| Publisher | : |
| Total Pages | : 1366 |
| Release | : 1969 |
| Genre | : Aeronautics |
| ISBN | : |
Download NASA Contractor Report Book in PDF, ePub and Kindle
