Prediction of Precombustion Wall Pressure Distributions in Scramjet Engines
Author:
Affiliation:
1. Johns Hopkins University, Applied Physics Laboratory, Silver Spring, Md.
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Space and Planetary Science,Aerospace Engineering
Link
https://arc.aiaa.org/doi/pdf/10.2514/3.27782
Reference5 articles.
1. Review of scramjet propulsion technology.
2. The interaction of shock waves and heat addition in the design of supersonic combustors
3. Structure of Shock Waves in Cylindrical Ducts
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