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S04021
Ref S04021 : F-16XL ship #1 - CAWAP boundary layer rakes and hot film on left wing
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DIMENSIONS
High Definition PRINT
BACKLIT*
40 x 60 cm
15.7 x 23.6 inches
23.00 €
20.70 €
125.00 €
50 x 75 cm
19.7 x 29.5 inches
29.90 €
26.91 €
140.00 €
60 x 90 cm
23.6 x 35.4 inches
45.00 €
40.50 €
170.00 €
80 x 120 cm
31.5 x 47.2 inches
75.00 €
220.00 €
100 x 150 cm
39.4 x 59.1 inches
109.00 €
290.00 €
*Backlit is a translucent matter to apply in front of a neon light
Thème :
Aviation-NASA aircrafts-Prototypes
Description
:
This photo shows the boundary layer hot film and the boundary layer rakes on the left wing of NASA's single-seat F-16XL (ship #1) used for the Cranked-Arrow Wing Aerodynamic Project (CAWAP) at Dryden Flight Research Center, Edwards, California. The modified airplane features a delta ''cranked-arrow'' wing with strips of tubing along the leading edge to the trailing edge to sense static on the wing and obtain pressure distribution data. The right wing receives data on pressure distribution and the left wing has three types of instrumentation - preston tubes to measure local skin friction, boundary layer rakes to measure boundary layer profiles (the layer where the air interacts with the surfaces of a moving aircraft), and hot films to determine boundary layer transition locations. The program also gathered aero data on two wing planforms for NASA's High Speed Research Program. The first flight of CAWAP occurred on November 21, 1995, and the test program ended in April 1996.
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Last update Friday 26 April, 2024