Spike nozzle contour for optimum thrust-Reference-Cited by-同舟云学术

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Spike nozzle contour for optimum thrust

Published:1961-01 Issue: Volume:4 Page:92-101
ISSN:0032-0633
Container-title:Planetary and Space Science
language:en
Short-container-title:Planetary and Space Science

Author:

Rao G.V.R.

Publisher

Elsevier BV

Subject

Space and Planetary Science,Astronomy and Astrophysics

Reference4 articles.

1. Performance of Plug Nozzles for Turbojet and Rocket Exhausts;Krase,1959

2. Effect of Plug Design on Performance Characteristics of Convergent-Plug Exhaust Nozzles;Krull;NACA RM E54HO5,1954

3. Effect of Several Design Variables on Internal Performance of Convergent-Plug Exhaust Nozzles;Krull;NACA RM E56G20,1956

4. Exhaust Nozzle Contour for Optimum Thrust

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1. Development and simulation of a 3D printed liquid oxygen/liquid natural gas aerospike;Acta Astronautica;2024-03

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3. CFD Analysis on Cooling of Conical Plug Aerospike Nozzle with Secondary Fluid Injection;Lecture Notes in Mechanical Engineering;2024

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