Continuation method for calculation of transonic airfoil flutter boundaries

Journal of Guidance, Control, and Dynamics

Volumn 20, Issue 6, 1997, Pages 1165-1171

  Beran, Philip S ^a,c,d   Morton, Scott A ^b,d,e,f  

^a AIR FORCE INSTITUTE OF TECHNOLOGY   (United States)

^b AIR FORCE RESEARCH LABORATORY   (United States)

^c Air Force Institute of Technology   (United States)

^d AIAA   (United States)

^e USAF   (United States)

^f Building 450   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

AIRFOILS; ALGORITHMS; FLIGHT DYNAMICS; SENSITIVITY ANALYSIS; TIME DOMAIN ANALYSIS; TRANSONIC AERODYNAMICS;

EULER EQUATION; MACH NUMBER; NACA 64A006 AIRFOIL; PSEUDOARCLENGTH CONTINUATION ALGORITHM; TRANSONIC AIRFOIL FLUTTER BOUNDARIES;

FLUTTER (AERODYNAMICS);

EID: 0031268484     PISSN: 07315090     EISSN: 15333884     Source Type: Journal    
DOI: 10.2514/2.4172     Document Type: Article

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