Induced aerodynamics from thrust vectoring are investigated by a computational fluid dynamic method. A thin-layer Reynolds-averaged Navier-Stokes code with multiblock capability is used. Jet properties are specified on the nozzle exit plane to simulate the jet momentum. Results for a rectangular jet in a cross flow are compared with data to verify the code. Further verification of the calculation is made by comparing the numerical results with transonic data for a wing-body combination. Additional calculations were performed to elucidate the following thrust vectoring effects: the thrust vectoring effect on shock and expansion waves, induced effects on nearby surfaces, and the thrust vectoring effect on the leading edge vortex. Tseng, Jing-Biau and Lan, C. Edward Unspecified Center BODY-WING CONFIGURATIONS; COMPUTATIONAL FLUID DYNAMICS; CROSS FLOW; JET FLOW; NAVIER-STOKES EQUATION; THRUST VECTOR CONTROL; VORTICES; AVERAGE; ELASTIC WAVES; LEADING EDGES; MOMENTUM; REYNOLDS EQUATION...