Investigation of a semispan tilt-wing VTOL model to determine ground effect on full-span flaps used for yaw control in hovering /
Kalman J. Grunwald.

APA Citation

Grunwald, K. J., Langley Research Center., United States. National Aeronautics and Space Administration. (1966). Investigation of a semispan tilt-wing VTOL model to determine ground effect on full-span flaps used for yaw control in hovering. Washington, D.C.: National Aeronautics and Space Administration .

MLA Citation

Grunwald, Kalman J, Langley Research Center, and United States. National Aeronautics and Space Administration. Investigation of a Semispan Tilt-wing VTOL Model to Determine Ground Effect On Full-span Flaps Used for Yaw Control In Hovering. Washington, D.C.: National Aeronautics and Space Administration , 1966.