A Hypersonic Inlet Cowling Scheme Using Slit Flow to Realize Separation
A hypersonic, air inlet technology, applied in the combustion of the air inlet of the power unit, the arrangement/installation of the power unit, the power unit on the aircraft, etc., can solve the difficulty of increasing the flight resistance and the thermal protection of the projectile and fairing, etc. problems, to achieve the effect of low structural strength requirements, flexible shape design and small size
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[0041] The technical solutions in the embodiments of the present invention will be clearly and completely described below with reference to the accompanying drawings in the embodiments of the present invention. Obviously, the described embodiments are only a part of the embodiments of the present invention, not all of the embodiments. Based on the embodiments of the present invention, all other embodiments obtained by those of ordinary skill in the art without creative efforts shall fall within the protection scope of the present invention.
[0042] It should be noted that all directional indications (such as up, down, left, right, front, back, etc.) in the embodiments of the present invention are only used to explain the relationship between various components under a certain posture (as shown in the accompanying drawings). The relative positional relationship, the movement situation, etc., if the specific posture changes, the directional indication also changes accordingly. ...
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