Experimental and numerical investigation of transient starting of pre-evacuated exhaust diffuser in high altitude ground test
Authors:
- Sina AfkhamiSASina Afkhami
- Nematollah FouladiNFNematollah Fouladi
- Mahmoud Pasandideh FardMFMahmoud Pasandideh Fard
- 10 January 2023
- journal article
- research article
- Published by Elsevier in Aerospace Science and Technology
- Vol. 133
Abstract
No abstract availableKeywords
This publication has 19 references indexed in Scilit:
- Hydrogen fuel rocket engines simulation using LOGOS codeInternational Journal of Hydrogen Energy, 2014
- A study of the supersonic ejector–diffuser system with an inlet orificeAerospace Science and Technology, 2012
- Design and Analysis of a Second-Throat Exhaust Diffuser for Altitude SimulationJournal of Propulsion and Power, 2012
- Performance Evaluation of Second-Throat Diffuser for High-Altitude-Test FacilityJournal of Propulsion and Power, 2010
- Studies on the starting transient of a straight cylindrical supersonic exhaust diffuser: Effects of diffuser length and pre-evacuation stateInternational Journal of Heat and Fluid Flow, 2008
- Side-Load Phenomena in Highly Overexpanded Rocket NozzlesJournal of Propulsion and Power, 2004
- Comparison of Several Difference Schemes on 1D and 2D Test Problems for the Euler EquationsSIAM Journal on Scientific Computing, 2003
- Evaluation of the performance of supersonic exhaust diffuser using scaled down modelsExperimental Thermal and Fluid Science, 1998
- A survey of several finite difference methods for systems of nonlinear hyperbolic conservation lawsJournal of Computational Physics, 1978
- Methods for determining the performance of ejector-diffuser systems.Journal of Spacecraft and Rockets, 1966