F-16XL Supersonic Laminar Flow Control Model
Description This is a multiple exposure image of the F-16XL Supersonic Laminar Flow Control (SLFC) model in the Unitary Plan Wind Tunnel. This wind tunnel test was conducted to verify design pressure distributions for the SLFC flight experiment (see modified port wing) and to obtain simulator coefficients for stability and control investigations.
Credit: NASA/Sandie Gibbs
Image Number: LRC-1994-P-03046
Date: April 29, 1994
F-16XL Supersonic Laminar Flow Control Model
Description This is a multiple exposure image of the F-16XL Supersonic Laminar Flow Control (SLFC) model in the Unitary Plan Wind Tunnel. This wind tunnel test was conducted to verify design pressure distributions for the SLFC flight experiment (see modified port wing) and to obtain simulator coefficients for stability and control investigations.
Credit: NASA/Sandie Gibbs
Image Number: LRC-1994-P-03046
Date: April 29, 1994