Approximate subspace iteration for constructing internally balanced reduced order models of unsteady aerodynamic systems

37th AIAA/ASME/ASCE/AHS/ASC Structure, Structural Dynamics and Materials Conference

Volumn , Issue , 1996, Pages 1070-1085

  Baker, Myles L ^a   Mingori, D Lewis ^b   Goggin, Patrick J ^a  

^a BOEING COMPANY   (United States)

^b UNIVERSITY OF CALIFORNIA   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

AERODYNAMICS; AEROELASTICITY; ITERATIVE METHODS; STRUCTURAL DYNAMICS; VECTORS; APPROXIMATION THEORY; MATHEMATICAL MODELS; UNSTEADY FLOW;

AEROELASTIC ANALYSIS; COMPUTATIONAL COSTS; MODEL REDUCTION TECHNIQUES; ORDERS OF MAGNITUDE; REDUCED ORDER MODELS; SCHUR DECOMPOSITION; SUBSPACE ITERATIONS; UNSTEADY AERODYNAMICS;

FINITE ELEMENT METHOD; COMPUTATIONAL FLUID DYNAMICS;

APPROXIMATE SUBSPACE ITERATION; INTERNAL BALANCING; REDUCED ORDER BALANCED MODELS;

EID: 0029700456     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: 10.2514/6.1996-1441     Document Type: Conference Paper

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