Automated Design Optimization for the P2 and P8 Hypersonic Inlets
Author:
Affiliation:
1. Rutgers University, New Brunswick, New Jersey 089
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
http://arc.aiaa.org/doi/pdf/10.2514/2.2161
Reference22 articles.
1. Advanced Transonic Fan Design Procedure Based on a Navier–Stokes Method
2. Aerodynamic shape optimization of a subsonic inlet using 3-D Euler computation
3. Stochastic optimization applied to CFD shape design
4. Applications of genetic algorithm to aerodynamic shape optimization
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1. Discrete Adjoint Optimization of a Hypersonic Inlet;AIAA Journal;2020-06
2. Design and experimental study of a practical Osculating Inward Cone Waverider Inlet;Chinese Journal of Aeronautics;2016-12
3. Mitigation of Adverse Effects Caused by Shock Wave Boundary Layer Interactions through Optimal Wall Shaping;31st AIAA Applied Aerodynamics Conference;2013-06-22
4. Investigation of Attack Angle Character for Hypersonic Inlet;Advanced Materials Research;2012-02
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