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Latif, M.Z.A.A
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Latif, M.Z.A.A
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Latif, M.Z.A.A
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1
An analysis on 45° sweep tail angle for blended wing body aircraft to the aerodynamics coefficients by wind tunnel experiment
by
Ahmad, M.A
,
Latif
,
M.Z.A.A
,
Nasir, R.E.M
,
Romli F.I
,
Saad, M.R
,
Wisnoe, W.
Published 2017
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2
Aerodynamics of a blended wing body aircraft with close-coupled tail: Computational Fluid Dynamics simulations of two different tail sweep angle cases
by
Ahmad, M.A
,
Kuntjoro, W.
,
Latif
,
M.Z.A.A
,
Nasir, R.E.M
,
Shafari, N.A.H.M
,
Wisnoe, W.
Published 2018
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Related Subjects
Aerodynamics
Aerodynamic characteristics
Angle of attack
Blended wing body
Blended wing body aircrafts
Blockage correction
Coefficient of drag
Computational Fluid Dynamic
Drag
Flow control
High-speed wind tunnel
Lift
Lift drag ratio
Lift to drag ratio
Streamline curvature
Swept wings
Wind tunnel experiment
Wind tunnels
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