Numerical Investigation of the HIFiRE-2 Scramjet Flowpath-Reference-Cited by-同舟云学术

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Numerical Investigation of the HIFiRE-2 Scramjet Flowpath

Published:2013-01-05 Issue: Volume: Page:
ISSN:
Container-title:51st AIAA Aerospace Sciences Meeting including the New Horizons Forum and Aerospace Exposition
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Author:

Yentsch Robert¹,Gaitonde Datta¹

Affiliation:

1. Ohio State University

Publisher

American Institute of Aeronautics and Astronautics

Link

http://arc.aiaa.org/doi/pdf/10.2514/6.2013-119

Reference33 articles.

1. Flight Data Analysis of the HyShot 2 Scramjet Flight Experiment

2. AIAA Educational Series;Anderson J. D.,1801

3. 5Heiser,W.H.andPratt,D.T.,HypersonicAirbreathingPropulsion,AmericanInstituteofAeronauticsandAstronautics,1994.

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1. Flow and Combustion in a Scramjet Engine with Two Opposed Cavity Flameholders;AIAA AVIATION 2023 Forum;2023-06-08

2. Numerical modelling of hydrogen combustion phenomena in a dual-mode ramjet engine with cavity flameholder;AIAA SCITECH 2023 Forum;2023-01-19

3. Unsteady Numerical Analysis of a Dual-Mode Scramjet Combustor with a Cavity;TRANSACTIONS OF THE JAPAN SOCIETY FOR AERONAUTICAL AND SPACE SCIENCES;2023

4. Numerical Investigation of the Ramjet and Scramjet Operation Regimes of the HIFiRE-2 Combustion Chamber;Fluid Dynamics;2022-11-29

5. Computational Analysis of Unstart in Variable-Geometry Inlet;Journal of Propulsion and Power;2021-07

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