Automated redesign of the NASA P8 hypersonic inlet using numerical optimization-Reference-Cited by-同舟云学术

Automated redesign of the NASA P8 hypersonic inlet using numerical optimization

Published:1996-07-01 Issue: Volume: Page:
ISSN:
Container-title:32nd Joint Propulsion Conference and Exhibit
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Author:

Shukla Vijay¹,Gelsey Andrew¹,Schwabacher Mark¹,Smith Donald¹,Knight Doyle¹

Affiliation:

1. Rutgers Univ., New Brunswick, NJ

Publisher

American Institute of Aeronautics and Astronautics

Link

http://arc.aiaa.org/doi/pdf/10.2514/6.1996-2549

Reference11 articles.

1. Stochastic optimization applied to CFD shape design

2. Nonlinear Optimization A nonlinear programming [Vanderplaats 1984, More and Wright 1993, Gill et al. 1981] problem consists ofa nonlinear objective function to be minimized, and a set of nonlinear constraints. It can be expressed as

3. 7.344e-2 1.1611e3 99.64 1.0 irest memmode iilemode residmode cpumode

4. 1 1 1 1 3 7 0 ng iseq nsweep ncycle nwres mstg rtolr rtola

5. 1 1 1 1 3 7 0

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