Write a Technical Report.

Laboratory experiment about investigate the variation in pressure around the aerofoil at different angles of incidence and the resultant effect on lift coefficient. The particular aerofoil to be tested is a symmetrical, constant cross-section RA 104 airfoil of 10% thickness. 1- Introduction about fundamental operation of an aerofoil (100 words mix) 2- The job is to compare between 6 tables recorded and convert the data to Si units. 3- Produce a plot of CL (Coefficient Lift) versus angle of incidence. 4- Present the Reynolds number associated with the test. 5- Provide discussion of (the effect of increasing the angle of incidence, the distribution of pressure around the aerofoil, and on the lift coefficient) 6- Discuss the contribution of estimated potential measurement error on variation in the derived results. Note: the results (Excel files is done only needs converts to Si units)