Flight Test and Evaluation of Fluidic Flight Control

Format:

Conference/Event

Author/Creator:

Keyser, David R., author.

Conference Name:

Aerospace Technology Conference & Exposition (1987-10-05 : Long Beach, California, United States)

Language:

English

Physical Description:

1 online resource

Place of Publication:

Warrendale, PA SAE International 1987

Summary:

This paper presents the results of a multi-year project by the Naval Air Development Center to design, fabricate, evaluate, and flight test a fluidic flight control system in a Navy T-2C, a twin-jet carrier aircraft. The work leading to this flight test began with component design to the aircraft installation constraints and to flight requirements, continued through fabrication, laboratory testing and system installation, and culminated with man-in-the-loop evaluation of the system installed in the aircraft, ground tests, and flight. The results of these tests demonstrate the successful integration of three advanced technologies:controlled both bywhich the Naval Air Development Center has brought to fruition

Notes:

Vendor supplied data

Publisher Number:

871864

Access Restriction:

Restricted for use by site license