Benchmarking the prediction of dynamic derivatives: Wind tunnel tests, validation, acceleration methods

AIAA Atmospheric Flight Mechanics Conference 2010

Volumn , Issue , 2010, Pages

  Mialon, B ^a   Khrabrov, A ^b   Da Ronclr, A ^c   Cavagna, Luca ^d   Zhang, Mengmeng ^e   Ricci, Sergio ^f  

^a ONERA   (France)

^b CENTRAL AEROHYDRODYNAMIC INSTITUTE TSAGI   (Russian Federation)

^c UNIVERSITY OF LIVERPOOL   (United Kingdom)

^d SWEDISH DEFENCE RESEARCH AGENCY   (Sweden)

^e ROYAL INSTITUTE OF TECHNOLOGY   (Sweden)

^f POLITECNICO DI MILANO   (Italy)

Author keywords

[No Author keywords available]

Indexed keywords

AIRCRAFT CONFIGURATIONS; DYNAMIC WIND TUNNEL TESTS; LARGE AMPLITUDE OSCILLATION; LINEAR AERODYNAMIC MODEL; NON-LINEAR AERODYNAMICS; SMALL-AMPLITUDE OSCILLATIONS; UNSTEADY REYNOLDS-AVERAGED NAVIER-STOKES; WING-FUSELAGE-TAIL CONFIGURATION;

AIRCRAFT MODELS; COMPUTATIONAL FLUID DYNAMICS; DYNAMICS; FLIGHT DYNAMICS; FUSELAGES; TOOLS; TRANSPORT AIRCRAFT; WIND STRESS;

AERODYNAMIC CONFIGURATIONS;

EID: 84880915129     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: None     Document Type: Conference Paper

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