Mesh strategies for accurate computation of unsteady spoiler and aeroelastic problems

Journal of Aircraft

Volumn 37, Issue 3, 2000, Pages 521-525

  Bartels, Robert E ^a  

^a NASA LANGLEY RESEARCH CENTER   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

AERODYNAMICS; COMPUTER SIMULATION; DYNAMIC RESPONSE; PROBLEM SOLVING; RELAXATION PROCESSES; STIFFNESS; UNSTEADY FLOW;

FLUID DOMAIN CONVERGENCE; MOVING SPOILER SURFACES;

AIRFOILS;

EID: 0033715583     PISSN: 00218669     EISSN: None     Source Type: Journal    
DOI: 10.2514/2.2629     Document Type: Article

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