NASA NTRS · 20000045999
Analysis and Multipoint Design of the TCA Concept
Abstract
The goal in this effort is to analyze the baseline TCA concept at transonic and supersonic cruise, then apply the natural flow wing design concept to obtain multipoint performance improvements. Analyses are conducted with OVERFLOW, a Navier-Stokes code for overset grids, using PEGSUS to compute the interpolations between the overset grids.
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Krist, Steven E., Bauer, Steven X. S., Buning, Pieter G.. 1999-12-01. Analysis and Multipoint Design of the TCA Concept. https://ntrs.nasa.gov/citations/20000045999
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