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NACA-TR-597
Air propellers in yaw
Year: 1937
Abstract: Report presents the results of tests conducted at Stanford University of a 3-foot model propeller at four pitch settings and at 0 degree, 10 degrees, 20 degrees, and 30 degrees yaw. In addition to the usual propeller coefficients, cross-wind and vertical forces and yawing, pitching, and rolling moments were determined about axes having their origin at the intersection of the blade axis and the axis of rotation. The tests showed that the maximum efficiency was reduced only slightly for angles of yaw up to 10 degrees but that at 30 degrees yaw the loss in efficiency was about 10 percent. In all cases the cross-wind force was found to be greater than the cross-wind component of the axial thrust. With a yawed propeller an appreciable thrust was found for v/nd for zero thrust at zero yaw. Yawing a propeller was found to induce a pitching moment that increased in magnitude with yaw.
Subject: AIRCRAFT
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| contributor author | NASA - National Aeronautics and Space Administration (NASA) | |
| date accessioned | 2017-09-04T15:23:19Z | |
| date available | 2017-09-04T15:23:19Z | |
| date copyright | 01/01/1937 | |
| date issued | 1937 | |
| identifier other | ATWUYDAAAAAAAAAA.pdf | |
| identifier uri | https://yse.yabesh.ir/std/handle/yse/23535 | |
| description abstract | Report presents the results of tests conducted at Stanford University of a 3-foot model propeller at four pitch settings and at 0 degree, 10 degrees, 20 degrees, and 30 degrees yaw. In addition to the usual propeller coefficients, cross-wind and vertical forces and yawing, pitching, and rolling moments were determined about axes having their origin at the intersection of the blade axis and the axis of rotation. The tests showed that the maximum efficiency was reduced only slightly for angles of yaw up to 10 degrees but that at 30 degrees yaw the loss in efficiency was about 10 percent. In all cases the cross-wind force was found to be greater than the cross-wind component of the axial thrust. With a yawed propeller an appreciable thrust was found for v/nd for zero thrust at zero yaw. Yawing a propeller was found to induce a pitching moment that increased in magnitude with yaw. | |
| language | English | |
| title | NACA-TR-597 | num |
| title | Air propellers in yaw | en |
| type | standard | |
| page | 15 | |
| status | Active | |
| tree | NASA - National Aeronautics and Space Administration (NASA):;1937 | |
| contenttype | fulltext | |
| subject keywords | AIRCRAFT | |
| subject keywords | EFFICIENCY | |
| subject keywords | MANEUVERS | |
| subject keywords | MOMENTS | |
| subject keywords | PITCH | |
| subject keywords | PITCHING | |
| subject keywords | PROPELLER | |
| subject keywords | PROPELLERS | |
| subject keywords | ROLLING | |
| subject keywords | TESTS | |
| subject keywords | TUNNEL | |
| subject keywords | VARIABLE | |
| subject keywords | WIND | |
| subject keywords | YAW | |
| subject keywords | YAWING |