Flight Dynamic Response of HALE Aircraft to KC-135 Flowfield

By Amanda J Devuono

This research effort examines the static affects of a KC-135 flowfield on a flexible winged Sensorcraft model. The KC-135 flowfield data is generated by a vortex lattice code and integrated into Sensorcraft model for analysis. Building on previous research, a refueling situation was modeled to note the effects of the Sensorcraft at varying locations within the flowfield. The Sensorcraft model was analyzed for both rigid and flexible wings as a means of comparision. Flowfield locations of interest were determined and trimmed conditions were computed for each flowfield location.

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• Format: Hardcover
• Language: English
• ISBN: 102509090X
• ISBN13: 9781025090900
• Release Date: May 2025
• Publisher: Hutson Street Press
• Length: 80 Pages
• Weight: 0.64 lbs.
• Dimensions: 0.3" x 6.1" x 9.2"