CPC G01P 5/16 (2013.01) [B64D 43/02 (2013.01)] | 15 Claims |
1. An aircraft configured to collect air data, the aircraft comprising:
a wing structure;
a forebody, forward of the wing structure;
an afterbody, backward of the forebody;
a skin covering the wing, the forebody and the afterbody;
at least one recess formed at the skin, the recess being configured to affect the pressure of air flowing at the recess;
at least one ambient sensor port for measuring ambient air pressure at the skin; and
at least one recess sensor port for measuring the air pressure at the recess.
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