Quasi-one-dimensional modeling of pressure effects in supersonic nozzles-Reference-Cited by-同舟云学术

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Quasi-one-dimensional modeling of pressure effects in supersonic nozzles

Published:2017-11 Issue: Volume:70 Page:161-169
ISSN:1270-9638
Container-title:Aerospace Science and Technology
language:en
Short-container-title:Aerospace Science and Technology

Author:

Maicke Brian A.^ORCID,Bondarev George

Publisher

Elsevier BV

Subject

Aerospace Engineering

Reference23 articles.

1. Steam Turbines;Stodola,1905

2. Numerical investigation of flow transition behavior in cold flow dual-bell rocket nozzles;Génin;J. Propuls. Power,2016

3. Unsteady shock motions in an over-expanded parabolic rocket nozzle;Verma;Aerosp. Sci. Technol.,2014

4. SSME/Side Loads Analysis for Flight Configuration;Holland,1974

5. LE-7A engine nozzle problems during the transient operations;Watanabe,2002

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1. On the Thrust Vector Performance Optimization and Modeling of Supersonic Split Line Nozzles;2024

2. Physical simulation of aerodynamic flow characteristics in a vertical diffuser with air supply through different pipe configurations;Power engineering: research, equipment, technology;2023-06-09

3. Experimental analysis of aerodynamic characteristics in the Hyperloop system;Aerospace Science and Technology;2023-06

4. Mathematical Description of the Aerodynamic Characteristics of Stationary Flows in a Vertical Conical Diffuser When Air Is Supplied through Various Tube Configurations;Axioms;2023-02-27

5. Empirical equation of the Mach number as a function of the stagnation pressure ratio for a quasi-one-dimensional compressible flow;FME Transactions;2023

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