An advanced buffet load alleviation system

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

Volumn 5, Issue , 2001, Pages 3579-3588

  Burnham, J K ^a   Pitt, D M ^a   White, E V ^a   Henderson, D A ^a   Moses, R W ^a  

^a BOEING COMPANY   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

ACTUATORS; AERODYNAMICS; AIRCRAFT MATERIALS; COMPUTER SIMULATION; DYNAMIC RESPONSE; FINITE ELEMENT METHOD; MULTIVARIABLE CONTROL SYSTEMS; PIEZOELECTRIC DEVICES; RUDDERS;

AEROSERVOELASTIC MODEL; AIRCRAFT VERTICAL TAILS; BUFFET LOAD ALLEVIATION SYSTEM; OSCILLATORY AERODYNAMICS; PIEZOELECTRIC ACTUATORS; STRUCTURAL DYNAMIC RESPONSE;

DYNAMIC LOADS;

EID: 0035021466     PISSN: 02734508     EISSN: None     Source Type: Conference Proceeding    
DOI: None     Document Type: Conference Paper

References (13)