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Includes the Committee's Technical reports no. 1-1058, reprinted in v. 1-37.
It is found that the impulse of each shed vortex and its image vortex in a transformed circle plane enters into all the interference forces and moments on the airplane. A simple theorem is given for the interference forces in steady straight flight which are found to depend on this impulse evaluated only at the wing trailing edge and at the base of the configuration.
Instrument-flying trials have been conducted in a single-rotor helicopter to determine the adequacy of existing longitudinal flying-qualities requirements under instrument conditions. In addition, laterial directional characteristics were examined. The suitability, for helicopter use, of standard airplane insruments was also investigated.
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