Inverse design of nacelles using multi-block Navier Stokes codes | Zendy

D. A. Naik | Zendy; S. Krist | Zendy; R. Campbell | Zendy; Veer N. Vatsa | Zendy; P. G. Buning | Zendy; Lie-Mine Gea | Zendy

AI Assistant Blog Pricing

Home ZAIA Blog

Open Access

Inverse design of nacelles using multi-block Navier Stokes codes

Author(s) -

D. A. Naik,

S. Krist,

R. Campbell,

Veer N. Vatsa,

P. G. Buning,

Lie-Mine Gea

Publication year - 1995

Publication title -

14th applied aerodynamics conference

Language(s) - English

Resource type - Conference proceedings

DOI - 10.2514/6.1995-1820

Subject(s) - computer science , nacelle , inverse , block (permutation group theory) , mathematics , engineering , aerospace engineering , combinatorics , geometry , turbine

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.

The content you want is available to Zendy users.

Already have an account? Click here to sign in.

Having issues? You can contact us here

Accelerating Research