Three-dimensional simulation of STS ignition overpressure-Reference-Cited by-同舟云学术

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Three-dimensional simulation of STS ignition overpressure

Published:1984-06-25 Issue: Volume: Page:
ISSN:
Container-title:17th Fluid Dynamics, Plasma Dynamics, and Lasers Conference
language:
Short-container-title:

Author:

BUELL J.¹

Affiliation:

1. Aerospace Corp., Fluid Mechanics Dept., El Segundo, CA

Publisher

American Institute of Aeronautics and Astronautics

Link

http://arc.aiaa.org/doi/pdf/10.2514/6.1984-1629

Reference4 articles.

1. Godunov, S. K., Zabrodin, A. V., and Prokopov, G. P."A Difference Scheme for Two-Dimensiona1 Unsteady Problems of Gas Dynamics and Camputation of Flow With A Detached Shock Wave," -Zh. vych. mat.: No. 6, 1020-1058, 1961; also Cornell Aero-Lab Translation (AD614916).

Cited by 8 articles. 订阅此论文施引文献订阅此论文施引文献，注册后可以免费订阅5篇论文的施引文献，订阅后可以查看论文全部施引文献

1. Numerical Study of Solid-Rocket Motor Ignition Overpressure Wave Including Infrared Radiation;Journal of Propulsion and Power;2014-01

2. CFD Simulations of Launch Environments for Delta IV Vehicles at the SLC-6 Launch Pad;49th AIAA Aerospace Sciences Meeting including the New Horizons Forum and Aerospace Exposition;2011-01-04

3. CFD analysis of unsteady ignition overpressure effects on Delta II and III launch vehicles;18th Applied Aerodynamics Conference;2000-08-14

4. Numerical investigation of inviscid shock wave dynamics in an expansion tube;Shock Waves;1995-06

5. A computational fluid dynamics analysis of the internal flow in a Titan SRMU;26th Joint Propulsion Conference;1990-07-16

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