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Volumn 47, Issue 2, 2010, Pages 450-457

Mechanism for warp-controlled twist of a morphing wing

Author keywords

[No Author keywords available]

Indexed keywords

ANGLE OF ATTACK; CRYSTAL LATTICES; DRAG; LIFT; LIFT DRAG RATIO; THIN WALLED STRUCTURES; WIND TUNNELS;

EID: 77950584616     PISSN: 00218669     EISSN: 15333868     Source Type: Journal    
DOI: 10.2514/1.39328     Document Type: Article
Times cited : (105)

References (24)
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  • 3
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    • Phillips, W.F.1
  • 4
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    • AIAA Paper 2005-1034, Reno, NV, Jan
    • Phillips, W. F., Fugal, S. R., and Spall, R. E., "Minimizing Induced Drag with Geometric and Aerodynamic Twist, CFD Validation," 43rd AIAA Aerospace Sciences Meeting and Exhibit, AIAA Paper 2005-1034, Reno, NV, Jan. 2005.
    • (2005) 43rd AIAA Aerospace Sciences Meeting and Exhibit
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  • 5
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    • Feb, doi:10.2514/3.46677
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  • 8
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    • doi:10.2514/2.2208
    • Andersen, G., Forster, E., Kolonay, R., and Eastep, F., "Multiple Control Surface Utilization in Active Aeroelastic Wing Technology," Journal of Aircraft, Vol. 34, No. 4, 1997, pp. 552-557. doi:10.2514/2.2208
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  • 9
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  • 12
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* 이 정보는 Elsevier사의 SCOPUS DB에서 KISTI가 분석하여 추출한 것입니다.