Numerical validation of a stability model for a flexible over-expanded rocket nozzle-Reference-Cited by-同舟云学术

Numerical validation of a stability model for a flexible over-expanded rocket nozzle

Published:2005 Issue:4 Volume:49 Page:349-369
ISSN:0271-2091
Container-title:International Journal for Numerical Methods in Fluids
language:en
Short-container-title:Int. J. Numer. Meth. Fluids

Author:

Lefrançois E.

Publisher

Wiley

Subject

Applied Mathematics,Computer Science Applications,Mechanical Engineering,Mechanics of Materials,Computational Mechanics

Reference36 articles.

1. . Numerical study of the starting process in a supersonic nozzle. CIMNE, West East High Speed Flow Fields, Barcelona 11-15, 2002.

2. Editors

3. Flow processes in overexpanded chemical rocket nozzles—Part I. NASA Report-77396, 1984.

4. . Fluctuating pressure analysis of a 2-D SSME nozzle air flow test. Workshop for Computational Fluid Dynamic Applications in Rocket Propulsion and Launch Vehicle Technology, Huntsville, Alabama, 26 April, 1995.

5. European Seminar on Rocket Nozzle Flows, 1998.

Cited by 15 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. Element-Quality-Based Stiffening for the Pseudoelastic Mesh-Moving Technique;International Journal of Computational Methods;2019-11-29

2. Numerical Experiment of Aeroelastic Stability for a Rocket Nozzle;Journal of Aerospace Engineering;2017-09

3. Adaptation of the Transpiration Method to Simulate the Fluid–Structure Interaction Phenomena for a Flexible Overexpanded Rocket Nozzle;30th International Symposium on Shock Waves 1;2017

4. New Modified Pekkari Model to Analyse the Aeroelastic Stability Behaviour for a Flexible Overexpanded Rocket Nozzle;30th International Symposium on Shock Waves 1;2017

5. Aeroelastic stability analysis of a flexible over-expanded rocket nozzle using numerical coupling by the method of transpiration;Journal of Fluids and Structures;2015-07