Aerospace Engineering > GATE 2017 > Aircraft Performance
A conventional low speed aircraft had the following aerodynamic characteristics:
CDO=0.020, e=1.0 (Oswald efficiency). The aircraft was flown to maintain a steady level flight and for minimum thrust required, at a lift coefficient of CL=0.8. The numerical value of the aspect ratio of the wing is _______ (in three decimal places).
CDO=0.020, e=1.0 (Oswald efficiency). The aircraft was flown to maintain a steady level flight and for minimum thrust required, at a lift coefficient of CL=0.8. The numerical value of the aspect ratio of the wing is _______ (in three decimal places).
Correct : 10.000 to 10.500
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