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NASA NTRS · 20000058104

TLNS3D/CDISC Multipoint Design of the TCA Concept

Abstract

This paper presents the work done to date by the authors on developing an efficient approach to multipoint design and applying it to the design of the HSR TCA configuration. While the title indicates that this exploratory study has been performed using the TLNS3DMB flow solver and the CDISC design method, the CDISC method could have been used with any flow solver, and the multipoint design approach does not require the use of CDISC. The goal of the study was to develop a multipoint design method that could achieve a design in about the same time as 10 analysis runs.

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BibTeXRIS

Campbell, Richard L., Mann, Michael J.. 1999-12-01. TLNS3D/CDISC Multipoint Design of the TCA Concept. https://ntrs.nasa.gov/citations/20000058104

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