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Investigation of Boundary Layer Control to Helicopter Rotor Blades.
NACA and Don Richey1957-01-22
NASA
Washington, DC, United States
Experimental investigation of boundary layer control to helicopter rotor blades to increase forward speed capabilities. 3/4 overhead view. Shaft angle - 35deg.
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Details
- Title: Investigation of Boundary Layer Control to Helicopter Rotor Blades.
- Creator: NACA, Don Richey
- Date Created: 1957-01-22
- Location: Ames Research Center
- Rights: ARC
- Album: drichey
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