Integral-Rocket Dual-Combustion Ramjets: A New Propulsion Concept
Author:
Affiliation:
1. The Johns Hopkins University Applied Physics Laboratory, Laurel, Md.
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Space and Planetary Science,Aerospace Engineering
Link
https://arc.aiaa.org/doi/pdf/10.2514/3.57760
Reference17 articles.
1. Structure of Shock Waves in Cylindrical Ducts
2. Prediction of Precombustion Wall Pressure Distributions in Scramjet Engines
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