NASA Technical Reports Server (NTRS) : Pressure pdf

NASA Technical Reports Server (NTRS) : Pressure

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Description of the Book:

Pressure distributions on a 1- by 3-meter semispan wing with a tip that is streamwise at 0 deg sweep are presented. The tip becomes nonstreamwise as the wing is swept. At 0 deg sweep angle, the semispan wing has a taper ratio of 1.0 and NACA 0012 airfoil section contours. The test was conducted in the Langley V/STOL tunnel at a freestream dynamic pressure of 2.46 kPa. Pressure distributions are presented for sweep angles of 10, 20, 30, and 40 with an angle of attack range from -6 deg to 20 deg. The data are presented without analysis or discussion

• Creator/s: NASA Technical Reports Server (NTRS
• Date: 8/1/1977
• Year: 1977
• Book Topics/Themes: NASA Technical Reports Server (NTRS), PRESSURE DISTRIBUTION, SEMISPAN MODELS, SUBSONIC FLOW, SWEPT WINGS, ANGLE OF ATTACK, SWEEP ANGLE, V/STOL AIRCRAFT, WIND TUNNEL TESTS, Yip, L. P., Shubert, G. L

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