Thermodynamic Analysis of Dual-Mode Scramjet Engine Operation and Performance
Author:
Affiliation:
1. University of Missouri - Rolla
2. NASA Langley Research Center
Publisher
American Institute of Aeronautics and Astronautics
Link
http://arc.aiaa.org/doi/pdf/10.2514/6.2006-8059
Reference13 articles.
1. Curran, E. T., and Stull, F. D. "The Utilization of Supersonic Combustion Ramjet Systems at Low Mach Numbers", Aero Propulsion Laboratory, RTD-TDR-63-4097, Jan.1964.
2. The interaction of shock waves and heat addition in the design of supersonic combustors
3. Prediction of Precombustion Wall Pressure Distributions in Scramjet Engines
4. Structure of Shock Waves in Cylindrical Ducts
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