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Latif, ZAA
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Latif, ZAA
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Latif, ZAA
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1
Experimental result analysis for scaled model of UiTM tailless blended wing-body (BWB) Baseline 7 unmanned aerial vehicle (UAV)
by
IOP
,
Ahmad, AM
,
Kuntjoro, W
,
Latif
,
ZAA
,
Nasir, REM
,
Saad, RM
Published 2017
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2
Aerodynamic characteristics of a cranked planform blended wing-body aircraft with 40° sweep angle
by
Ahmad, A.M
,
Ishak, I.S
,
Kuntjoro, W.
,
Latif
,
Z.A.A
,
Nasir, R.E.M
,
Wisnoe, W.
Published 2018
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3
Experimental result analysis for scaled model of UiTM tailless blended wing-body (BWB) Baseline 7 unmanned aerial vehicle (UAV)
by
Ahmad, A.M
,
Kuntjoro, W.
,
Latif
,
Z.A.A
,
Nasir, R.E.M
,
Romli F.I
,
Saad, R.M
Published 2017
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Related Subjects
Aerodynamics
Aerodynamic configurations
Aerodynamic drag
Angle of attack
Angle of attack indicators
Automobile bodies
Blended wing body
Blended wing body aircrafts
Blended-wing body
Drag
Experimental aerodynamics
Fighter aircraft
Flat surfaces
Flow control
Future perspectives
Lift
Lift drag ratio
Lift to drag ratio
Maximum lift coefficient
Planforms
Result analysis
Scaled modeling
Unmanned aerial vehicles (UAV)
Wind tunnel test
Wind tunnels
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