DocumentCode
343942
Title
F/A-18A/B/C/D 9G flight test program
Author
Long, Jennifer ; Koyama, L. T William
Author_Institution
Aircraft Div., Naval Air Warfare Center, Patuxent River, MD, USA
Volume
3
fYear
1999
fDate
1999
Firstpage
111
Abstract
The purpose of the 9g flight test program recently conducted at Naval Air Warfare Center Aircraft Division, Patuxent River, was to investigate the capability of the F/A-18A/B/C/D aircraft for a 9g load factor envelope (a 1.5g increase over current capability). The 9g capability was enabled by a patch to the mission computer software which changed the basic g-limiter function, including the transonic load factor decrement, or “g bucket” function. The flight test had four objectives: to demonstrate component loads less than 100% design limit for the 9g flight envelope; to evaluate vertical tail buffet during 9g maneuvers; to test the functionality of the g-limiter for 9g maneuvers; and to demonstrate satisfactory flying qualities for the 9g envelope. The paper contains a detailed discussion of problems encountered and lessons learned during the flight test
Keywords
aircraft control; aircraft testing; military aircraft; military avionics; F/A-18A/B/C/D 9G flight test program; F/A-18A/B/C/D aircraft; fighter aircraft; g bucket function; g-limiter function; load factor envelope; mission computer software; transonic load factor decrement; vertical tail buffet; Aircraft propulsion; Engines; Instruments; Military aircraft; Military computing; Rivers; Sea surface; Strain measurement; Tail; Testing;
fLanguage
English
Publisher
ieee
Conference_Titel
Aerospace Conference, 1999. Proceedings. 1999 IEEE
Conference_Location
Snowmass at Aspen, CO
Print_ISBN
0-7803-5425-7
Type
conf
DOI
10.1109/AERO.1999.789771
Filename
789771
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