Aeroshape design and low speed aerodynamic analysis of a crew return vehicle

This publication has 17 references indexed in Scilit:

• Multi-disciplinary optimization of a space re-entry vehicle using skeleton-based integral soft objects
  Aerospace Science and Technology, 2022
• An optimal heat-flux targeting procedure for LEO re-entry of reusable vehicles
  Aerospace Science and Technology, 2021
• Low speed longitudinal aerodynamics of a blended wing-body re-entry vehicle
  Aerospace Science and Technology, 2020
• Aeroshape design of reusable re-entry vehicles by multidisciplinary optimization and computational fluid dynamics
  Aerospace Science and Technology, 2020
• Constraint-based parameterization using FFD and multi-objective design optimization of a hypersonic vehicle
  Aerospace Science and Technology, 2020
• An aerothermodynamic design optimization framework for hypersonic vehicles
  Aerospace Science and Technology, 2018
• Multi-objective optimization for re-entry spacecraft conceptual design using a free-form shape generator
  Aerospace Science and Technology, 2017
• Free topology generation of self-stiffened panels using skeleton-based integral soft objects
  Computers & Structures, 2015
• Optimization of entry-vehicle shapes during conceptual design
  Acta Astronautica, 2014
• A parameterized geometry design method for inward turning inlet compatible waverider
  Chinese Journal of Aeronautics, 2013