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The flow past a straight and a swept-wing-body combination and their equivalent bodies of revolution at Mach numbers near 1.0.

Author
Lindsey, Walter F
Physical Description
1 electronic document
Online Version

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Summary
Tests utilizing the Schlieren method of flow photography have been conducted to provide a comparison of the complete flow fields past a straight and a swept-wing-body combination and the flow fields past their equivalent bodies of revolution at Mach numbers around 1.0. The results indicated that the shock growth and positions on the wing-body combinations were closely reproduced in the flow past the equivalent body.
Collection
NASA Technical Reports Server (NTRS) Collection.
Note
Document ID: 19930093724.
Accession ID: 93R23016.
NACA-RM-L54A28a.
Terms of Use and Reproduction
No Copyright.
View MARC record | catkey: 15428468