Aerodynamic effects induced from vectoring an exhaust jet are investigated using a well established thin-layer Reynolds averaged Navier-Stokes code. This multiple block code has been modified to allow for the specification of jet properties at a block face. The applicability of the resulting code for thrust vectoring applications is verified by comparing numerically and experimentally determined pressure coefficient distributions for a jet-wing afterbody configuration with a thrust-vectoring 2-D nozzle. Induced effects on the body and nearby wing from thrust vectoring are graphically illustrated.
Numerical Simulation of Propulsion-Induced Aerodynamic Characteristics on a Wing-Afterbody Configuration with Thrust Vectoring
Sae Technical Papers
Aerospace Atlantic Conference & Exposition ; 1991
01.04.1991
Aufsatz (Konferenz)
Englisch
Evaluation and Application of VSAERO to a Nonaxisymmetric Afterbody with Thrust Vectoring
SAE Technical Papers | 1987
|Aerodynamic thrust vectoring of jets
AIAA | 1995
|