Paper information

Paper code

IAC-21,C4,IP,3,x66560

Order

1003

Room

IP Area

Title

Computational Analysis of Boundary layer in Dual Throat Nozzle with secondary injection.

abstract

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Session

IP. Interactive Presentations - IAF SPACE PROPULSION SYMPOSIUM

symposium

C4. IAF SPACE PROPULSION SYMPOSIUM

congress

IAC-21

Type of presentation

interactive

Main author

Ms. Deeksha K, R V College of Engineering, Bengaluru, India

Co-authors

Mr. Raj Kedia, R.V.College of Engineering, India;

Ms. Shreesha Madhu, Valles Marineris International Private Limited, India;