Which of the following is done to reduce the static defect?
(a) Streamlined configuration of the whole aircraft
(b) Less weight as payload
(c) Wind tunnel tests to find spots of body-flow interference
(d) Deploy Flaps and slats
The question was asked by my college director while I was bunking the class.
The query is from Pressure Measurements topic in section Air Data Systems, Altitude and Heading Reference of Avionics