Investigation At Transonic Speeds Of The Loading Over A 45 Degree Sweptback Wing Having An Aspect Ratio Of 3 A Taper Ratio Of 02 And Naca 65a004 Airfoil Sections PDF Download
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| Author | : Jack F. Runckel |
| Publisher | : |
| Total Pages | : 104 |
| Release | : 1956 |
| Genre | : Aerodynamic load |
| ISBN | : |
Download Investigation at Transonic Speeds of the Loading Over a 45 Degree Sweptback Wing Having an Aspect Ratio of 3, a Taper Ratio of 0.2, and NACA 65A004 Airfoil Sections Book in PDF, ePub and Kindle
An investigation at transonic speeds of the loading over a 45 degree sweptback wing having an aspect ratio of 3, a taper ratio of 0.2, and NACA 65A004 airfoil sections has been conducted in the Langley16-foot transonic tunnel. Pressure measurements on the wing-body combination were obtained at angles of attack from 0 to 26 degrees at Mach numbers from 0.80 to 0.98 and from 0 to about 12 degrees at Mach numbers from 1.00 to 1.05. Reynolds number, based on the wing mean aerodynamic chord, varied from 7,000,000 to 8,500,000 over the test Mach number range.
| Author | : United States. National Aeronautics and Space Administration |
| Publisher | : |
| Total Pages | : 448 |
| Release | : 1960 |
| Genre | : Aeronautics |
| ISBN | : |
Download Index of NASA Technical Publications Book in PDF, ePub and Kindle
| Author | : F. E. West |
| Publisher | : |
| Total Pages | : 76 |
| Release | : 1960 |
| Genre | : |
| ISBN | : |
Download Effect of Body-mounted Lateral Controls and Speed Brakes on the Aerodynamic Load Distribution Over a 45 Degree Swept Wing at Mach Numbers from 0.80 to 0.98 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 | : United States. National Aeronautics and Space Administration |
| Publisher | : |
| Total Pages | : |
| Release | : 1960-07 |
| Genre | : |
| ISBN | : |
Download Index to NASA Technical Publications Book in PDF, ePub and Kindle
| Author | : Donald D. Arabian |
| Publisher | : |
| Total Pages | : 88 |
| Release | : 1960 |
| Genre | : Aerodynamics, Transonic |
| ISBN | : |
Download Investigation at Transonic Speeds of Loading Over a 30 Deg Sweptback Wing of Aspect Ratio 3, Taper Ratio 0.2, and NACA 65A004 Airfoil Section Mounted on a Body Book in PDF, ePub and Kindle
The aerodynamic load characteristics of a wing-body combination were determined experimentally at Mach numbers from 0.80 to 1.03 for angles of attack up to 26 degrees. Two wings, both with 30 degrees sweep of the quarter-chord line, taper ratio of 0.2, aspect ratio of 3, and thickness of 4 percent chord, but of different types of construction, were tested. One wing was of solid steel and the other was of plastic with an inner steel core ...
| Author | : |
| Publisher | : |
| Total Pages | : 1878 |
| Release | : 1961 |
| Genre | : Government publications |
| ISBN | : |
Download Monthly Catalog of United States Government Publications Book in PDF, ePub and Kindle
| Author | : Jack F. Runckel |
| Publisher | : |
| Total Pages | : 98 |
| Release | : 1961 |
| Genre | : Aerodynamics |
| ISBN | : |
Download Investigation at Transonic Speeds of the Loading Over a 40 Degree Sweptback Wing Having an Aspect Ratio of 3, a Taper Ratio of 0.2 and NACA 65A004 Airfoil Sections Book in PDF, ePub and Kindle
| Author | : Charles F. Whitcomb |
| Publisher | : |
| Total Pages | : 286 |
| Release | : 1961 |
| Genre | : |
| ISBN | : |
Download An Investigation of Wing and Aileron Loads Due to Deflected Inboard and Outboard Ailerons on a 4-percent-thick 30 Degree Swepptback Wing at Transonic Speeds Book in PDF, ePub and Kindle
| Author | : |
| Publisher | : |
| Total Pages | : 1096 |
| Release | : 1961 |
| Genre | : Mechanics, Applied |
| ISBN | : |
Download Applied Mechanics Reviews Book in PDF, ePub and Kindle
