The objective of this work is to reshape a nacelle to achieve a specified nacelle pressure distribution. The nacelle may be either isolated or installed on an airplane. There are no restrictions on the attitude (toe, incidence, and roll) and position of the nacelle. The design algorithm is coupled to two different multi-block 3-D Navier Stokes flow solvers. The coupling between design and analysis is automated to the point where the design proceeds with minimal user input.
Inverse Design of Nacelles Using Multi-Block Navier Stokes Codes
1995-01-01
Miscellaneous
No indication
English
Navier-Stokes Calculations For Transport Wing-Body Configurations with Nacelles and Struts
British Library Conference Proceedings | 1993
|Efficient constrained design using Navier-Stokes codes
AIAA | 1995
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