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two-dimensional and symmetrical about and hypersonic - lufteinlauf for the combustion air of a flugzeugmotors.
two-dimensional and symmetrical about and hypersonic - lufteinlauf for the combustion air of a flugzeugmotors.
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机译:二维和对称的高超声速-lufteinlauf用于flugzeugmotors的燃烧空气。
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The bidimensional supersonic and hypersonic air intake for the combustion air of an aircraft engine comprises two forward flaps (3) forming a visor, which are disposed symmetrically on either side of a longitudinal plane (P), each forward flap (3) being movable about a pivot axis (4) situated in the vicinity of the wall of the air intake which extends the forward flap under consideration. The pivot axis (4) of each forward flap (3) is situated in the vicinity of a first boundary layer trap (5) disposed in the wall of the air intake which extends said forward flap (3). …IMAGE…
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