22nd Congress of International Council of the Aeronautical Sciences, Harrogate, UK, 28 August - 1st September, 2000
Paper ICAS 2000-5.2.1
CIVIL AIRCRAFT ENGINE INTAKES WITH NEGATIVE SCARF INSPIRED BY REQUIREMENTS FOR ACOUSTIC REDUCTIONS - PRELIMINARY, AERODYNAMIC PERFORMANCE ASSESSMENT
R. K. Nangia, M. E. Palmer
Nangia Aero Research Associates, Bristol, UK
Keywords: aircraft engine intake, negative scarf, acoustic reduction
Aircraft engines must meet current and future
FAR regulations and noise "footprints" criteria.
A way of reducing noise is to use negatively
scarfed inlets. The extended lower lip acts as an
acoustic "barrier". We need to understand the
aerodynamic implications of inlet scarfing at
low and transonic speeds.
The subsonic aerodynamic performance
(incidence, side-slip and ground effects) of a
conventional (+6° scarf) inlet has been
assessed. A range of negative scarf angles was
applied to the geometry and the subsonic
performance of the resulting inlets assessed. A
staged, iterative design process was carried out
on a -20° scarfed inlet from this series. This led
to modified lip geometry that gave attached flow
capability equivalent to the datum
"conventional" inlet. An additional advantage
for negative scarf was the weakening of the
ground vortex at "zero forward speed". This is
important for "large" intakes with high by-pass
ratios, set closer to the ground.
The transonic performance of the
conventional (+6° scarf) and negatively scarfed
inlet (-20°) was assessed. A limited design study
was carried out on the -20° inlet to understand
the effects of lip shaping at high speed (Mach
0.8). An encouraging equivalence has been
achieved between the datum and scarfed inlet
and further detailed work (internal surfaces)
leading to experiments has been recommended.
Work is needed on scarf angle choice.
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