Gust loads alleviation using special control surfaces

Journal of Aircraft

Volumn 44, Issue 1, 2007, Pages 17-25

  Moulin, B ^a,b,c   Karpel, M ^a,c,d  

^a TECHNION ISRAEL INSTITUTE OF TECHNOLOGY   (Israel)

^b Faculty of Aerospace Engineering   (Israel)

^c AIAA   (United States)

^d Faculty of Aerospace Engineering

Author keywords

[No Author keywords available]

Indexed keywords

AIRCRAFT; BENDING MOMENTS; CONTROL THEORY; FORCE CONTROL; LOW PASS FILTERS; WIND TUNNELS;

AEROELASTIC EFFECTIVENESS; GUST-ALLEVIATION LOOP; WIND-TUNNEL MODELS;

LOADS (FORCES);

EID: 33847746682     PISSN: 00218669     EISSN: 15333868     Source Type: Journal    
DOI: 10.2514/1.19876     Document Type: Article

References (9)

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8. Karpel, M., Moulin, B., and Chen, P. C., "Dynamic Response of Aeroservoelastic Systems to Gust Excitation," Journal of Aircraft, Vol. 42, No. 5, 2005, pp. 1264-1272.
9. Karpel, M., Moulin, B., Anguita, L., Maderuelo, C., and Climent, H., "Aeroservoelastic Gust Response Analysis for the Design of Transport Aircrafts," AIAA Paper 2004-1592, April 2004.