Plume-Ducting System Design of Vertical Launcher Using Computational-Fluid-Dynamics Tools-Reference-Cited by-同舟云学术

Plume-Ducting System Design of Vertical Launcher Using Computational-Fluid-Dynamics Tools

Published:2013-05 Issue:3 Volume:50 Page:715-718
ISSN:0022-4650
Container-title:Journal of Spacecraft and Rockets
language:en
Short-container-title:Journal of Spacecraft and Rockets

Author:

Saha S.¹,Chakraborty Debasis¹

Affiliation:

1. Defence Research and Development Laboratory, Hyderabad 500 058, India

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.A32303

Reference6 articles.

1. BertinJ. J.KorstH. H. “Launch-Tube Flow-Field Technology Based on Cold-Gas Simulations, Flight-Test Measurements and Theoretical Models,” Fluid Dynamics Lab., Univ. of Texas Rept. 83-102, Austin, TX, April 1983.

2. The launch-tube flow-field for a vertical launching system

3. Rocket Exhaust Flow in Tube Launchers

4. Supersonic Jet Impingement Navier-Stokes Computations for Vertical Launching System Design Applications

5. also Paper No. 2A-3.

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