Question 40

AENAT2 marksNeeds review
A conventional low speed aircraft had the following aerodynamic characteristics:

,

(Oswald efficiency). The aircraft was flown to maintain a steady level flight and for minimum thrust required, at a lift coefficient of

. The numerical value of the aspect ratio of the wing is ____________ (in three decimal places).

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2017AE

GATE AE 2017 · Paper 1

Aerospace Engineering · Original paper archive

Section
Aerospace Engineering
Question type
Numerical answer (NAT)
Marks
2 marks

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