Maximum control surface freeplay, design and flight testing approach on the F-22

Collection of Technical Papers - AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics and Materials Conference

Volumn 1, Issue , 2007, Pages 767-778

  Anderson, William D ^a,c,d   Mortara, Sean ^b,e  

^a LOCKHEED MARTIN   (United States)

^b WRIGHT PATTERSON AIR FORCE BASE   (United States)

^c F 22 Structures IPT ^*  (United States)

^d AIAA   (United States)

^e Bldg 553

Author keywords

[No Author keywords available]

Indexed keywords

CONSERVATIVE DESIGN; FLIGHT TESTING; FREEPLAY; HINGE MOMENT;

COMPUTER SIMULATION; FLIGHT CONTROL SYSTEMS; HINGES; MANEUVERABILITY; METHOD OF MOMENTS; STRUCTURAL DYNAMICS;

FLUTTER (AERODYNAMICS);

EID: 34547535263     PISSN: 02734508     EISSN: None     Source Type: Conference Proceeding    
DOI: None     Document Type: Conference Paper

References (5)

1. th AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics, and Materials Conference, 2007 (to be published).
2. th ed., Dover Publications Inc., Mineola, NY, 1985, Chap. 8, ISBN 0-486-64785-4.
3. Joint Service Specification Guide 2006, Wright-Patterson AFB, OH, 1998.
4. Guruswamy, G. P., and Byun, C., "Fluid-Structural Interactions Using Navier-Stokes Flow Equations Coupled with Shell Finite Element Structures", AIAA-93-3087.
5. Anderson, W. D., Transonic Buzz - W/T Test and ENSAERO Analysis Comparison, Aerospace Flutter & Dynamics Council, Monterey, CA, 9-10 Oct, 2003.