Some Factors of Hypersonic Inlet/Airplane Interactions
Author:
Affiliation:
1. Russian Academy of Sciences, Novosibirsk, 630090, Russia
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
http://arc.aiaa.org/doi/pdf/10.2514/2.2922
Reference33 articles.
1. Inlet Boundary-Layer Shapes on Four Aircraft Forebodies at Mach 6
2. Mach 6 flowfield survey at the engine inlet of a research airplane
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1. Airframe- Configuration Effect on Condition of Airflow to Engine in Hypersonic Flow;Journal of Propulsion and Power;2007-09
2. Computational Analysis of Inlet Aerodynamics for a Hypersonic Research Vehicle;Journal of Propulsion and Power;2005-03
3. Reynolds Averaged Navier-Stokes Based Aerodynamic Analysis of Inlet for a Hypersonic Research Vehicle;12th AIAA International Space Planes and Hypersonic Systems and Technologies;2003-12-15
4. Effect of Airframe Configuration on Airflow Condition to Engine in Hypersonic Flow;21st AIAA Applied Aerodynamics Conference;2003-06-21
5. Inlets and Nozzles;The Scramjet Engine
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