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Investigation of Boundary Layer Control to Helicopter Rotor Blades. | Cosmos Observatory | Cosmos Observatory

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Investigation of Boundary Layer Control to Helicopter Rotor Blades.

Investigation of Boundary Layer Control to Helicopter Rotor Blades.

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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Keywords

Helicopter Boundary Layer 40x80ft Wind Tunnel Ames ARC Aeronautics

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Details

NASA ID

A-22383_1

Date Created

January 22, 1957

Center

ARC

Media Type

image

Photographer

NACA

Location

Ames Research Center

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Boundary-Layer Control to Helicopter Rotor Blades.

Jan 22, 1957