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Studying nonlinear surface behavior with the deep channel surface viscometer

✍ Scribed by Madhukar G Hegde; John C Slattery


Book ID
103154658
Publisher
Elsevier Science
Year
1971
Tongue
English
Weight
476 KB
Volume
35
Category
Article
ISSN
0021-9797

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NONLINEAR BEHAVIOR OF A TYPICAL AIRFOIL
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A three degree-of-freedom aeroelastic typical section with control surface freeplay is modeled theoretically as a system of piecewise linear state-space models . The system response is determined by time marching of the governing equations using a standard Runge -Kutta algorithm in conjunction with