Research

Astronomy & Space Sciences

Title :

Investigation of launch vehicle base flow-field in presence of supersonic under expanded multijet 6 environment at various external free stream flow conditions

Area of research :

Astronomy & Space Sciences

Focus area :

Aerodynamic Design and Analysis

Contact info :

Details

Executive Summary :

The highly underexpanded jet in multijet environment causes significant upstream influence. This results in changes in pressure distribution on the core as well as strap-on boosters.

Co-PI:

Shri Vinod Kumar, Vikram Sarabhai Space Centre (VSSC), Thiruvananthapuram

Organizations involved