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
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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