Static aeroelastic control of an adaptive lifting surface

Autor:	Steven M. Ehlers, Terrence A. Weisshaar
Rok vydání:	1993
Předmět:	Airfoil Wing root Engineering Wing business.industry Aerospace Engineering Structural engineering Aeroelasticity Lift (force) Control theory Control system Dynamic pressure business Actuator
Zdroj:	Journal of Aircraft. 30:534-540
ISSN:	1533-3868 0021-8669
DOI:	10.2514/3.46376
Popis:	Piezoelectric actuators are embedded in an idealized laminated composite wing structure that can adapt to changing flight conditions. A feedback control system senses wing roots strains and then applies a proportional voltage to active actuator layers to change wing lift or divergence dynamic pressure
Databáze:	OpenAIRE
Externí odkaz:	https://explore.openaire.eu/search/publication?articleId=doi_________::84e8dd8d71955949d1bee7265e3c2c2d https://doi.org/10.2514/3.46376 Zobrazit plný text záznamu