最終更新日:2022/12/24
The separation of the flow over wings precipitated by the compression shock that forms as speeds are increased into the supercritical Mach number range has imposed serious difficulties in the improvement of aircraft performance. These difficulties arise principally as a consequence of the rapid drag rise and the loss of lift that causes serious stability changes when the wing shock-stalls.
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元となった例文
The
separation
of
the
flow
over
wings
precipitated
by
the
compression
shock
that
forms
as
speeds
are
increased
into
the
supercritical
Mach
number
range
has
imposed
serious
difficulties
in
the
improvement
of
aircraft
performance.
These
difficulties
arise
principally
as
a
consequence
of
the
rapid
drag
rise
and
the
loss
of
lift
that
causes
serious
stability
changes
when
the
wing
shock-stalls.