Ideal Heat Release of Supersonic Combustion
Author:
Affiliation:
1. School of Energy Science and Engineering, Harbin Institute of Technology, 150001 Heilongjiang, People’s Republic of China
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Space and Planetary Science,Mechanical Engineering,Fuel Technology,Aerospace Engineering
Link
http://arc.aiaa.org/doi/pdf/10.2514/1.B34735
Reference12 articles.
1. Review of Problems in Application of Supersonic Combustion
2. Two-Dimensional Model for Thermal Compression
3. OgorodnikovD. A.VinogradovV. A.ShikhmanY. M.StrokinV. N. “Design and Research Russian Program of Experimental Hydrogen Fueled Dual Mode Scramjet: Choice of Conception and Results of Pre-Flight Tests,” AIAA Paper 1998-1586, 1998.
4. Development and testing of the aerojet strutjet combustor
5. Dual-mode operation in a scramjet combustor
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2. Ideal Heat Release and Ideal Inner Configuration of Supersonic Combustor;Journal of Propulsion and Power;2018-03
3. Gas-dynamic problems in off-design operation of supersonic inlets (review);Thermophysics and Aeromechanics;2017-11
4. Comment on “Parametric Ideal Scramjet Cycle Analysis”;Journal of Thermophysics and Heat Transfer;2015-01
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