Case Study
Estimation of Inlet Flow Distortion for Supersonic Aircraft
© 2014 Zeus Numerix Pvt Ltd Ph +91 20 64731511 contact@zeusnumerix.com VERTICAL: AEROSPACE & DEFENCE SERVICE: ENGINEERING SERVICES TECHNOLOGY: CFD ESTIMATION OF INLET FLOW DISTORTION FOR SUPERSONIC AIRCRAFT Our customer is India’s largest aerospace organization engaged with design, fabrication and assembly of military aircrafts and jet engines. During aircraft high AOA steady flight, rapid maneuvering and departures (e