Investigation of a semispan tilting-propeller configuration and effects of ratio of wing chord to propeller diameter on several small-chord tilting-wing configurations at transition speeds /
Kenneth P. Spreemann.

APA Citation

Spreemann, K. P., Langley Research Center., United States. National Aeronautics and Space Administration. (1963). Investigation of a semispan tilting-propeller configuration and effects of ratio of wing chord to propeller diameter on several small-chord tilting-wing configurations at transition speeds. Washington, D.C.: National Aeronautics and Space Administration.

MLA Citation

Spreemann, Kenneth P, Langley Research Center, and United States. National Aeronautics and Space Administration. Investigation of a Semispan Tilting-propeller Configuration And Effects of Ratio of Wing Chord to Propeller Diameter On Several Small-chord Tilting-wing Configurations At Transition Speeds. Washington, D.C.: National Aeronautics and Space Administration, 1963.