from: Storming Media
Type of bind: Spiral-bound
EAN num: 9781423541219
ISBN number: 1423541219
Label: Storming Media
Manufacturer: Storming Media
Page Count: 84
Printing Date: 1999
Publishing house: Storming Media
Studio: Storming Media
Editor's Notes and Comments:
Product Description:
This is a NAVAL POSTGRADUATE SCHOOL MONTEREY CA report procured by the Pentagon and made available for public release. It has been reproduced in the best form available to the Pentagon. It is not spiral-bound, but rather assembled with Velobinding in a soft, white linen cover. The Storming Media report number is A516173. The abstract provided by the Pentagon follows: Low-speed wind tunnel tests were conducted to determine surface pressure measurements on a proposed aerodynamic fairing for the Altus II UAV. These tests were conducted at various angle-of-attack and sideslip positions to determine the effect on the surface pressures for the optical window portion of the fairing. Of particular interests were the pressure contour field located over the optical window region and the total force exerted on this area. Scaled- up loads (lbf) as calculated on the window ran from 1.0 to 1.6 times the freestream dynamic pressure (psf). Pressure measurements were also taken on the upper fuselage of the Altus II UAV model to determine the location of the peak suction area. These measurements provided the data to optimize the placement of external vents on the full-scale version of the airframe.
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