Component and Vehicle Aerodynamic Characteristics of a Low Aspect Ratio Winged Aerospace Vehicle Configuration

摘要

Component-wise aerodynamic characteristics of a low aspect ratio winged flight vehicle configuration has been investigated using an Euler CFD code and limited wind-tunnel tests and discussed in this paper. Interference factors K_W and K_B have been generated from the results. These will be used to augment the capability of an existing in-house rapid prediction code.