Effects of plunging motion on unsteady aerodynamic behavior of an aircraft model in compressible flow

Iranian Journal of Science and Technology, Transaction B: Engineering

Volumn 31, Issue 1, 2007, Pages 49-63

  Davari, A R ^a,b   Soltani, M R ^a,b  

^a ISLAMIC AZAD UNIVERSITY   (Iran)

^b SHARIF UNIVERSITY OF TECHNOLOGY   (Iran)

Author keywords

Hysteresis loop; Pitch damping derivative; Pitching motion; Plunging motion; Stability derivative

Indexed keywords

AERODYNAMICS; AIRCRAFT; COMPRESSIBLE FLOW; FLOW FIELDS; MACH NUMBER; MATHEMATICAL MODELS; UNSTEADY FLOW;

AERODYNAMICS; AIRCRAFT; COMPRESSIBLE FLOW; HYSTERESIS; UNSTEADY FLOW; WIND TUNNEL;

EID: 34248596218     PISSN: 03601307     EISSN: None     Source Type: Journal    
DOI: None     Document Type: Article

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