Actions for Computation of transonic viscous flow past the NTF 65-degree Delta Wing

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Computation of transonic viscous flow past the NTF 65-degree Delta Wing

Author
Wu, Chivey
Published
Dec 1, 1993.
Physical Description
1 electronic document
Online Version

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Unclassified, Unlimited, Publicly available.
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Summary
This project is a continuation of the work performed in the summers of 1991 and 1992, during which a 9-block structured grid for the computational domain around each of the four NTF 65-degree Delta Wing models with the sting mount were created. The objective of the project is to validate and supplement the test data on the wing models by computing the viscous flow field about the models.
Other Subject(s)
Collection
NASA Technical Reports Server (NTRS) Collection.
Note
Document ID: 19940023427.
Accession ID: 94N27930.
Old Dominion Univ., The 1993 NASA-ODU American Society for Engineering Education (ASEE) Summer Faculty Fellowship Program; p 196-199.
Terms of Use and Reproduction
No Copyright.
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