A numerical investigation of side-loads resulting from rigid body motions of an overexpanded engine nozzle-Reference-Cited by-同舟云学术

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A numerical investigation of side-loads resulting from rigid body motions of an overexpanded engine nozzle

Published:2010-01-28 Issue:6 Volume:66 Page:671-689
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

Link

http://onlinelibrary.wiley.com/wol1/doi/10.1002/fld.2268/fullpdf

Reference42 articles.

1. Numerical investigation of transient nozzle flow;Mouronval;International Journal of Shock Waves,2003

2. Kudryavtsev A Hadjadj A Visualisation graphique en mécanique des fluides

3. Jacobs PA Simulation of transient flow in a shock tunnel and a high Mach number nozzle

4. Shock pattern in the plume of rocket nozzles: needs for design consideration;Hagemann;Shock Waves,2008

5. Jean F Alliot P Development status of the VINCI engine for Ariane 5 upper stage

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1. Equivalent Structural Modeling Using Laminated Composite Shell Analysis for the Nozzle Component of a Launch Vehicle Engine;Journal of Aerospace Engineering;2018-11

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

3. 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

4. Aeroelastic stability analysis of flexible overexpanded rocket nozzle;Shock Waves;2015-05-21

5. Combined interface boundary condition method for fluid–rigid body interaction;Computer Methods in Applied Mechanics and Engineering;2012-06

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