Cryogenic Fluid Injection and Mixing at Supercritical Conditions-Reference-Cited by-同舟云学术

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Cryogenic Fluid Injection and Mixing at Supercritical Conditions

Published:2003-01-06 Issue: Volume: Page:
ISSN:
Container-title:41st Aerospace Sciences Meeting and Exhibit
language:
Short-container-title:

Author:

Zong Nan¹,Meng Hua¹,Yang Vigor¹

Affiliation:

1. Pennsylvania State University

Publisher

American Institute of Aeronautics and Astronautics

Link

http://arc.aiaa.org/doi/pdf/10.2514/6.2003-480

Reference25 articles.

1. G.N.Abramovich,Thetheoryofturbulentjets (MITPress,Cambridge, 1963).

2. Characterization of cryogenic injection at supercritical pressure

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1. Simulation of unsteady combustion in a LOX-GH2 fueled rocket engine;Aerospace Science and Technology;2009-12

2. Mass transfer and combustion in transcritical non-premixed counterflows;Combustion Theory and Modelling;2009-01-22

3. SUPERCRITICAL FLUIDS: NANOTECHNOLOGY AND SELECT EMERGING APPLICATIONS;Combustion Science and Technology;2006-01

4. Transcritical oxygen/transcritical or supercritical methane combustion;Proceedings of the Combustion Institute;2005-01

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