NUMERICAL AND EXPERIMENTAL STUDY OF FLUIDIC THRUST VECTORING IN A CONVERGING-DIVERGING NOZZLE USING SHOCK VECTOR CONTROL
Date
Journal Title
Journal ISSN
Volume Title
Publisher
I.O.E
Abstract
Description
Fluidic thrust vectoring via Shock Vector Control (SVC) offers an efficient alternative to
traditional mechanical systems by utilizing secondary flow injection to deflect primary
supersonic jet exhaust.