Publisher's Synopsis
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. Naik, D. A. and Krist, S. E. and Campbell, R. L. and Vatsa, V. N. and Buning, P. G. and Gea, L. M. Ames Research Center; Langley Research Center AIAA Paper 95-1820 NAS1-19672...
