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| Author | : |
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| Total Pages | : 174 |
| Release | : 1969 |
| Genre | : Rotors (Helicopters) |
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| Author | : Cornell Aeronautical Laboratory |
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| Total Pages | : |
| Release | : 1969 |
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| Author | : CORNELL AERONAUTICAL LAB INC BUFFALO N Y. |
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| Total Pages | : 312 |
| Release | : 1969 |
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Contents: Model vs. full scale rotor testing; The flow throughout a wind tunnel containing a rotor with a sharply deflected wake; Comments on V/STOL wind tunnel data at low forward speeds; Problems associated with tunnel tests of high disk loading systems at low forward speeds; Some research on rotor circulation control; The aerodynamics of a circulation-controlled rotor; Higher harmonic pitch control; and The controllable twist rotor.
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| Total Pages | : 100 |
| Release | : 1969 |
| Genre | : Rotors (Helicopters) |
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| Author | : |
| Publisher | : |
| Total Pages | : 186 |
| Release | : 1969 |
| Genre | : Rotors (Helicopters) |
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| Author | : |
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| Total Pages | : 792 |
| Release | : 1970 |
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| Author | : |
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| Total Pages | : 64 |
| Release | : 1986 |
| Genre | : Aeronautics |
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| Author | : United States. National Aeronautics and Space Administration Scientific and Technical Information Division |
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| Total Pages | : 966 |
| Release | : 1970 |
| Genre | : Aeronautics |
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| Author | : Harry H. Heyson |
| Publisher | : |
| Total Pages | : 340 |
| Release | : 1970 |
| Genre | : Short take-off and landing aircraft |
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Under sufficiently large wake deflections, the forward portion of the wake is found to flow forward along the floor leading to a vortex pattern which results in Rae's limits (Journal of Aircraft, May-June 1967). Although wind-tunnel data cannot normally be corrected successfully beyond these limits, it may be possible to obtain ground-effect data for conditions more severe than those implied by Rae.
| Author | : Cornell University. Cornell Aeronautical Laboratory |
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| Release | : 1969 |
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