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Thrust vectoring characteristics of the F-18 high alpha research vehicle at angles of attack from 0 to 70 deg (1992)

Asbury, Scott C. ; Capone, Francis J.

In: Other Sources

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Publication Date: 2019-06-28

Description: An investigation was conducted to determine the multiaxis thrust-vectoring characteristics of the F-18 High Alpha Research Vehicle (HARV). A 0.10-scale model was modified with hardware to simulate the three-vane thrust vectoring system of the F-18/HARV. This investigation was conducted at Mach numbers ranging from 0.30 to 0.70, at angles of attack from 0 to 70 deg, and nozzle-pressure ratios from 2.0 to approximately 5.0. Results indicate that the thrust vectoring system of F-18/HARV can successfully generate multiaxis thrust vectoring. During vectoring, resultant thrust-vector angles were always less than the corresponding geometric vane deflection angle and were accompanied by large thrust losses.

Keywords: AIRCRAFT STABILITY AND CONTROL

Type: AIAA PAPER 92-3095

Format: text

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