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Estimating Methods, Variability, and Sampling for Drop-Test Data

Results (Continued)

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Graphical (Continued)

Contour plot of drop 204 (12:17 p.m., July 12, 2001). Flight direction: north to south. Aircraft elevation: 145 feet. Windspeed: 5 miles per hour. Low-flow rate: 250 gallons of water per second. GTS-R density: 1.097 grams per cubic centimeter.

Figure 12—Contour plot of drop 204 after triangulation.


Contour plot of drop 205 (2:56 p.m., July 12, 2001). Flight direction: north to south. Aircraft elevation: 155 feet. Windspeed: o to 5 miles per hour. Medium-flow rate: 500 gallons of water per second. GTS-R density: 1.096 grams per cubic centimeter.

Figure 13—Contour plot of drop 205 after triangulation.


Contour plot of drop 206 (3:38 p.m., July 12, 2001). Flight direction: north to south. Aircraft elevation: 160 feet. Windspeed: 4 miles per hour. Medium-flow rate: 500 gallons of water per second. GTS-R density: 1.095 grams per cubic centimeter.

Figure 14—Contour plot of drop 206 after triangulation.


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