DocumentCode
324442
Title
Flutter testing in the 90´s (The GBU-24 saga)
Author
Girard, Maj Maurice ; McIntosh, Capt Stuart
Author_Institution
Aircraft Div., Naval Air Warfare Center, Patuxent River, MD, USA
Volume
3
fYear
1998
fDate
21-28 Mar 1998
Firstpage
39
Abstract
Operation Desert Storm demonstrated the benefits of employing large guided penetrating weapons with long standoff ranges against hardened targets. The article concerns the GBU-24B/B laser-guided bomb (LGB). Before flight testing, a flutter analysis study indicated that certain CF-18/GBU-24 configurations exhibited 5.6 Hz antisymmetric flutter. It was therefore recommended that a flutter/limit cycle oscillation (LCO) flight test be conducted prior to fleet release of the GBU-24. Initial testing was completed using a production lot V CF-18B aircraft configured with symmetrical GBU-24s on the outboard wing stations, symmetrical external fuel tanks on the inboard wing stations, and symmetrical wing tip missiles. Flutter flight testing was temporarily suspended during the program after explosive flutter was encountered. The paper discusses the flight test approach, the buildup technique, the conduct of the tests up to and beyond this point as it evolved in the light of findings, the results and, most importantly, the lessons learned during the entire flutter flight test programs of the CF-18 in GBU-24 configurations
Keywords
aerospace testing; dynamic testing; laser beam applications; limit cycles; missile guidance; 5.6 Hz; 5.6 Hz antisymmetric flutter; CF-18B aircraft; GBU-24B/B laser-guided bomb; explosive flutter; flutter analysis; flutter testing; flutter/limit cycle oscillation flight test; large guided penetrating weapons; Aerodynamics; Aerospace engineering; Aerospace testing; Aircraft propulsion; Elasticity; Lakes; Missiles; Rivers; Storms; Weapons;
fLanguage
English
Publisher
ieee
Conference_Titel
Aerospace Conference, 1998 IEEE
Conference_Location
Snowmass at Aspen, CO
ISSN
1095-323X
Print_ISBN
0-7803-4311-5
Type
conf
DOI
10.1109/AERO.1998.685679
Filename
685679
Link To Document