Study of Conical Aerospike Nozzles with Base-Bleed and Freestream Effects
Author:
Affiliation:
1. College of Engineering Trivandrum, Kerala 695 016, India
2. Andong National University, Andong 760749, South Korea
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Space and Planetary Science,Aerospace Engineering
Link
https://arc.aiaa.org/doi/pdf/10.2514/1.A34256
Reference41 articles.
1. Advanced Rocket Nozzles
2. History of Liquid Propellant Rocket Engines
3. Spike nozzle contour for optimum thrust
4. Approximate method for plug nozzle design
5. Design of Maximum Thrust Plug Nozzles for Fixed Inlet Geometry
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