Aerodynamic benefits of adaptive wing technology

Aerospace Science and Technology

Volumn 4, Issue 7, 2000, Pages 439-452

  Stanewsky, Egon ^a  

^a Inst fur Stromungsmechanik   (Germany)

Author keywords

Adaptive wing; Boundary layers; Flow control; Shock waves; Transonic flow; Wing aerodynamics

Indexed keywords

EID: 0034357608     PISSN: 12709638     EISSN: None     Source Type: Journal    
DOI: 10.1016/S1270-9638(00)01069-5     Document Type: Article

References (38)

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