Longitudinal aerodynamic characteristics of a 1/30-scale subsonic canard-airplane model having a wing with an aspect ratio of 3.6 at mach numbers from 0.30 to 0.98.

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Summary

Wind tunnel aerodynamic characteristics of subsonic nuclear powered canard aircraft model

Other Subject(s)

Collection

NASA Technical Reports Server (NTRS) Collection.

Note

Document ID: 19650017036.
Accession ID: 65N26637.
NASA-TM-X-669.

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No Copyright.

View MARC record | catkey: 15959624