Measurements of the local heat transfer coefficients were made on a hemispherically convex surface with a round oblique impinging jet. The liquid crystal transient method was used for these measurements. This method, which is a variation on the transient method, suddenly exposes a preheated wall to an impinging jet while video recording the response of liquid crystal for the surface temperature measurements. The Reynolds number used was 23000 and the nozzle-to-surface distance was L/d=2, 4, 6, 8, and 10 and the jet angle was $alpha$=$0^{circ}; 15^{circ};30^{circ}C; and ;40^{circ}C$. In the experiment, the Nusselt number at the stagnation point decreases as the jet angle increases and has the maximum value for L/d=6. The X-axis Nusselt number distributions exhibit Secondary maxima at $0^{circ}C e $alpha$ e 15^{circ}C, L/dle6$</TEX> for X/d＜0(upstream) and at $0^{circ}C e $alpha$40^{circ}C,;L/dle4;and; at; 30^{circ}C e $alpha$$leq$40^{circ}C,;L/dle 6 $</TEX>for X/d＞0(downstream). The secondary maxima occurs at long distance from the stagnation point as the jet angle increases or the nozzle-to-surface distance decreases. The Y-axis Nusselt number distributions exhibit secondary maxima at Y/d=$pm$2 for $0^{circ}Cle ale30^{circ}C; and; L/dle4, and ;for;$alpha$=40^{circ}C$</TEX>and L/d=2. The displacement of the maximum Nusselt number from the stagnation point increases as the jet angle increases or the nozzle-to-surface distance decreases and the maximum distance is about 0.67 times of the nozzle diameter. The ratio of the maximum Nusselt number to the stagnation Nusselt number increases as the jet angle increases.