In Silico Studies on Truncated Aerospike Nozzle with Optimum Cowl Length for Single Stage to Orbit Vehicles

Autor: Shubhangi Sundaria, Amritansh Kumar Bhagat, VR Sanal Kumar
Rok vydání: 2023
Zdroj: 25th AIAA International Space Planes and Hypersonic Systems and Technologies Conference.
Databáze: OpenAIRE