Solution of reactive flow in a rocket engine nozzle with Paraffin/Kerosene propellants-Reference-Cited by-同舟云学术

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Solution of reactive flow in a rocket engine nozzle with Paraffin/Kerosene propellants

Published:2021-04-18 Issue:10 Volume:101 Page:
ISSN:0044-2267
Container-title:ZAMM - Journal of Applied Mathematics and Mechanics / Zeitschrift für Angewandte Mathematik und Mechanik
language:en
Short-container-title:Z. Angew. Math. Mech.

Author:

Nagler Jacob¹^ORCID

Affiliation:

1. School of Mechanical Engineering University of Tel‐Aviv Tel‐Aviv 69978 Israel

Publisher

Wiley

Subject

Applied Mathematics,Computational Mechanics

Link

https://onlinelibrary.wiley.com/doi/pdf/10.1002/zamm.202000074

Reference24 articles.

1. Thermodynamics and Chemical Kinetics of One‐Dimensional Nonviscous Flow through a Laval Nozzle

2. Atomic recombination in nozzles: methods of analysis for flows with complicated chemistry;Bray K.N.C.;Aero. Res. Counc., Lond., Rep. C.P.,1963

3. Chemical reactions in supersonic nozzle flows

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