In-flight tuning: Wind tunnel test results and flight test preparation

Annual Forum Proceedings - AHS International

Volumn 1, Issue , 2011, Pages 617-628

  Fuerst, Daniel ^a   Arnold, Uwe T P ^a   Graham, Douglas ^b  

^a ZF Luftfahrttechnik GmbH   (Germany)

^b Technology Manager Helitune Ltd   (United Kingdom)

Author keywords

[No Author keywords available]

Indexed keywords

FLIGHT TEST; PITCH LINKS; WIND TUNNEL TESTS;

FLIGHT SIMULATORS; HELICOPTERS; ION BEAMS; TESTING; WIND STRESS;

WIND TUNNELS;

EID: 79960657650     PISSN: 15522938     EISSN: None     Source Type: Conference Proceeding    
DOI: None     Document Type: Conference Paper

References (9)

1. Renzi, M.J., An Assessment of Modern Methods for Rotor Track and Balance, Master Thesis, Air Force Institute of Technology, Wright-Patterson Air Force Base, Ohio, June 2004.
2. Wang, S., et al., Adaptive Method of Helicopter Track and Balance, In Journal of Dynamic Systems, Measurement, and Control, Vol. 127, pp.275-282, June 2005.
3. th Annual Forum, Phoenix, Arizona, May, 2003.
4. Bechhoefer, E., Power D., IMD HUMS Rotor Track and Balance Techniques, In Proceeding Aerospace Conference Proceedings, pp. 3205-3211, 2003.
5. th Annual Forum, Grapevine, TX, May, 2009.
6. Haber, A., Jacklin, S.A., and deSimone, G., "Development, Manufacturing, and Component Testing of an Individual Blade Control System for a UH-60 Helicopter Rotor," American Helicopter Society Aerodynamics, Acoustics, and Test and Evaluation Technical Specialists Meeting, San Francisco, CA, January 2002
7. Arnold, U.T.P., Fuerst, D., "Closed loop IBC results from CH-53G flight tests", Aerospace Sciences and Technology, Vol. 9, pp. 421-435, 2005
8. SAE AS5394, Health and Usage Monitoring System, Advanced Multipoint Interface Specification.
9. SAE ARP 4761, Guidelines and Methods for Conducting the Safety Assessment Process on Civil Airborne Systems and Equipment.