Air at point (1) is drawn into a small open-circuit wind tunnel as shown in the below figure. 27C. Atmospheric pressure is 98.7 kPa (abs) and the temperature is If viscous effects are negligible, determine the pressure at the stagnation point (2) on the nose of the determine manometer for the manometer attached to the static pressure tap within the test section of + Inlet Inlet nozzle O Test section Diffuser Water Fan