Aerospace Engineering > GATE 2020 > Stability and Control
For a general aviation airplane with tail efficiency η = 0.95, horizontal tail volume ratio VH = 0.453, downwash angle slope dε/dα = 0.35, wing lift curve slope CLαw = 4.8 rad-1, horizontal tail lift curve slope CLαt = 4.4 rad-1, shift in neutral point location as a percentage of mean aerodynamic chord is _______ (round off to two decimal places).
Correct : 25.60 to 25.70
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