Progressive aerodynamic model identification from dynamic water tunnel test of the F-16XL aircraft

Collection of Technical Papers - AIAA Atmospheric Flight Mechanics Conference

Volumn 2, Issue , 2004, Pages 1256-1275

  Murphy, Patrick C ^a,c   Klein, Vladislav ^b,c   Szyba, Nathan M ^b,c  

^a NASA LANGLEY RESEARCH CENTER   (United States)

^b GEORGE WASHINGTON UNIVERSITY   (United States)

^c Airborne Systems   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

ANGLE OF ATTACK; DYNAMIC WATER TUNNEL TEST; F-16XL AIRCRAFT; NONLINEAR UNSTEADY AERODYNAMICS;

AIRCRAFT; DAMPING; DATA REDUCTION; MATHEMATICAL MODELS; NATURAL FREQUENCIES; OSCILLATIONS; POLYNOMIALS; TRANSFER FUNCTIONS; TUNNELS;

FLIGHT DYNAMICS;

EID: 19644364148     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: None     Document Type: Conference Paper

References (29)

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