Detached-Eddy Simulation of Shock Unsteadiness in an Overexpanded Planar Nozzle-Reference-Cited by-同舟云学术

Detached-Eddy Simulation of Shock Unsteadiness in an Overexpanded Planar Nozzle

Published:2017-06 Issue:6 Volume:55 Page:2016-2028
ISSN:0001-1452
Container-title:AIAA Journal
language:en
Short-container-title:AIAA Journal

Author:

Martelli E.¹,Ciottoli P. P.²,Bernardini M.²,Nasuti F.²,Valorani M.²

Affiliation:

1. Second University of Naples, 81031 Aversa, Italy

2. University of Rome “La Sapienza”, 00184 Rome, Italy

Publisher

American Institute of Aeronautics and Astronautics (AIAA)

Subject

Aerospace Engineering

Link

https://arc.aiaa.org/doi/pdf/10.2514/1.J055273

Reference41 articles.

1. Sea level side loads in high-area-ratio rocket engines

2. OstlundJ. “Flow Process in Rocket Engine Nozzles with Focus on Flow Separation and Side-Loads,” Ph.D. Thesis, Royal Inst. of Technology, Mekanik, Stockholm, 2002.

3. Unsteadiness of Flow Separation and End-Effects Regime in a Thrust-Optimized Contour Rocket Nozzle

4. Numerical investigation of separated nozzle flows

5. Viscous and Inviscid Vortex Generation During Startup of Rocket Nozzles

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