Continuation of work published in Report No. 496 indexed in Engineering Index 1935 p 19, under heading Airplane Control Surfaces -- Flutter; results of that paper have been extended to include effect of aerodynamic balance and effect of tab added to aileron; aerodynamic coefficients presented in form convenient for application to flutter problem.
Nonstationary flow about Wing-Aileron-Tab combination including aerodynamic balance
Nat Advisory Committee Aeronautics -- Report
1942
10 pages
Report
Englisch
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