Shape Optimization for Hypersonic Arc-Wing Missiles
Author:
Affiliation:
1. Chinese Academy of Sciences, Beijing 100190, China
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Space and Planetary Science,Aerospace Engineering
Link
https://arc.aiaa.org/doi/pdf/10.2514/1.45882
Reference19 articles.
1. Trajectory optimization for hypersonic boost‐glide missile considering aeroheating
2. Genetic-Algorithm Optimization of Liquid-Propellant Missile Systems
3. A new procedure for aerodynamic missile designs using topological optimization approach of continuum structures
4. Multidisciplinary Design Optimization of a Built-Up Wing Structure with Tip Missile
5. Multidisciplinary Optimization of Airbreathing Hypersonic Vehicles
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1. Aerodynamic Shape Optimization of a Hypersonic Missile Geometry;25th AIAA International Space Planes and Hypersonic Systems and Technologies Conference;2023-05-27
2. Aerodynamic Shape Design of Hypersonic Vehicles via Interval-Robust Optimization Method Including Geometric Tolerances and Multiple Flight Conditions;Journal of Aerospace Engineering;2021-05
3. A preliminary multidisciplinary design procedure for tactical missiles;Proceedings of the Institution of Mechanical Engineers, Part G: Journal of Aerospace Engineering;2018-09-04
4. Uncertainty propagation in aerodynamic forces and heating analysis for hypersonic vehicles with uncertain-but-bounded geometric parameters;Aerospace Science and Technology;2018-06
5. High-Pressure Capturing Wing Configurations;AIAA Journal;2017-06
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