Numerical Simulation of Propulsion-Induced Aerodynamic Characteristics on a Wing-Afterbody Configuration with Thrust Vectoring NASA Langley Research Center

Format:

Conference/Event

Author/Creator:

Krist, Steven E., author.

Conference Name:

Aerospace Atlantic Conference & Exposition (1991-04-22 : Dayton, Ohio, United States)

Language:

English

Physical Description:

1 online resource

Place of Publication:

Warrendale, PA SAE International 1991

Summary:

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

Notes:

Vendor supplied data

Publisher Number:

911174

Access Restriction:

Restricted for use by site license