Investigation of Applied Methods for Flow Investigations on Wings of an Aircraft via MEMS Sensors

Flow control has been an interesting area of research for researchers in aerospace science over the years. As it is known, any proper control should be coupled with update information. Thus, the present work is to introduce a suitable method to prepare this information. A detailed review of 30 years of sensor development with the particular objective of flow control purpose has been done.The goal to this is to find a proper method to use MEMS-based sensors on the wings of an aircraft to gather enough data for active and instantaneous control of flow in the flight regime. New and old MEMS sensors have been categorized and with the help of the AHP method, the suitable parameter to be sensed is found and the method to do this is also found with the help of AHP. In the end, amongpresent sensors introduced by the scientists over the years, the best one is chosen.

کلیدواژه ها:

MEMS ، flow control ، sensor ، aircraft wing ، AHP