Basic Pressure Measurements At A Mach Number Of 143 On A Thin 45 Deg Sweptback Highly Tapered Wing With Systematic Spanwise Twist Variations PDF Download
Are you looking for read ebook online? Search for your book and save it on your Kindle device, PC, phones or tablets. Download Basic Pressure Measurements At A Mach Number Of 143 On A Thin 45 Deg Sweptback Highly Tapered Wing With Systematic Spanwise Twist Variations PDF full book. Access full book title Basic Pressure Measurements At A Mach Number Of 143 On A Thin 45 Deg Sweptback Highly Tapered Wing With Systematic Spanwise Twist Variations.
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| Total Pages | : 82 |
| Release | : 1960 |
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Download Basic Pressure Measurements at a Mach Number of 1.43 on a Thin 45 Deg Sweptback Highly Tapered Wing with Systematic Spanwise Twist Variations Book in PDF, ePub and Kindle
Pressure distributions are presented on four wings: an untwisted wing to serve as a reference, and wings with linear, quadratic and cubic twist variations along the span. All the twisted wings had 0deg twist at the 10-percent-semispan station and 6deg twist at the tip. The tests were made at a Mach number of 1.43 and covered an angle-of-attack range from -4deg to 20deg. The average Reynolds number based on the wing mean aerodynamic chord was 2.9 x 10(exp 6) during tests at a stagnation pressure of 1.0 atmosphere and 1.5 x 10(exp 6) during tests at a stagnation pressure of 0.5 atmosphere.
| Author | : John P. Mugler |
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| Total Pages | : 73 |
| Release | : 1960 |
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Download Basic Pressure Measurements at a Mach Number of 1.43 on a Thin 45° Sweptback Highly Tapered Wing with Systematic Spanwise Twist Variations Book in PDF, ePub and Kindle
| Author | : John P. Jr Mugler |
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| Total Pages | : 0 |
| Release | : 1960 |
| Genre | : Wall pressure (Aerodynamics) |
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Download Basic Pressure Measurements at a Mach Number of 1/43 on a Thing 45 Degree Sweptback Highly Tapered Wing with Systematic Spanwise Twist Variations Book in PDF, ePub and Kindle
Pressure distributions are presented on four wings: an untwisted wing to serve as a reference, and wings with linear, quadratic, and cubic twist variations along the span. All the twisted wings had 0 degrees twist at the 10-percent-semispan station and 6 degrees twist at he tip. The tests were made at a Mach number of 1.43 and covered an angle-of-attack range from -4 degrees to 20 degrees. The average Reynolds number based on the wing mean aerodynamic chord was 2.9 X 10(6) during tests at a stagnation pressure of 1.0 atmosphere and 1.5 X 10(6) during tests at a stagnation pressure of 0.5 atmosphere.
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| Total Pages | : 44 |
| Release | : 1959 |
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Download Effects of Three Spanwise Twist Variations on the Longitudinal Aerodynamic Characteristics of a Thin 45 Deg Sweptback Highly Tapered Wing at Transonic Speeds Book in PDF, ePub and Kindle
| Author | : Thomas L. Fischetti |
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| Total Pages | : 94 |
| Release | : 1957 |
| Genre | : Aerodynamic load |
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Download Investigation at Mach Numbers from 0.80 to 1.43 of Pressure and Load Distributions Over a Thin 45 Degree 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.
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| Total Pages | : 1386 |
| Release | : 1959 |
| Genre | : Aeronautics |
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Download Aero/space Engineering Book in PDF, ePub and Kindle
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| Total Pages | : 20 |
| Release | : 1963 |
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Download Pressure Distribution and Force and Moment Measurements of an 80 Deg Swept Wing with Twist and Camber at a Mach Number of 2.98 Book in PDF, ePub and Kindle
| Author | : Jack D. Stephenson |
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| Total Pages | : 86 |
| Release | : 1955 |
| Genre | : Aeronautics |
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Download A Comparison at Mach Numbers Up to 0.92 of the Calculated and Experimental Downwash and Wake Characteristics at Various Horizonatl Tail Heights Behind a Wing with 45 Degrees of Sweepback Book in PDF, ePub and Kindle
| Author | : H. Herbert Jackson |
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| Total Pages | : 32 |
| Release | : 1960 |
| Genre | : Mach number |
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Download Free-flight Measurements of the Zero-lift Drag of Several Wings at Mach Numbers from 1.4 to 3.8 Book in PDF, ePub and Kindle
| Author | : Frank J. Centolanzi |
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| Total Pages | : 82 |
| Release | : 1959 |
| Genre | : Mach number |
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Download Measured and Theoretical Flow Fields Behind a Rectangular and a Triangular Wing Up to High Angles of Attack at a Mach Number of 2.46 Book in PDF, ePub and Kindle
