Inlet Trade Study for a Low Boom Aircraft Demonstrator
Author:
Affiliation:
1. NASA Glenn Research Center
2. National Institute of Aerospace
Publisher
American Institute of Aeronautics and Astronautics
Link
http://arc.aiaa.org/doi/pdf/10.2514/6.2016-4050
Reference20 articles.
1. Propulsion/Airframe Integration and Optimization on a Supersonic Business Jet
2. Multidisciplinary Optimization of a Supersonic Inlet Using a Cartesian CFD Method
3. Under-Track CFD-Based Shape Optimization for a Low-Boom Demonstrator Concept
4. Inward-Turning Streamline-Traced Supersonic Inlet Design Method for Low-Boom, Low-Drag Applications
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