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

Implementing Organization

Vikram Sarabhai Space Centre (VSSC), Thiruvananthapuram
CO-Principal Investigator
Shri Vinod Kumar
Vikram Sarabhai Space Centre (VSSC), Thiruvananthapuram

Project Overview

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.

Related Research

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Funding Organization
Funding Organization
Department of Space (DoS)
Quick Information
Area of Research
Astronomy & Space Sciences
Focus Area
Aerodynamic Design and Analysis
Status
Ongoing
Output
No. of Research Paper
00
Technologies (If Any)
00
No. of PhD Produced
N/A
Startup (If Any)
00
No. of Patents
Filed :00
Grant :00
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